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wind tunnel

wind tunnel, Total:251 items.

In the international standard classification, wind tunnel involves: Road vehicles in general, Valves, Structure and structure elements, Geology. Meteorology. Hydrology, Aircraft and space vehicles in general, Internal combustion engines, Commercial vehicles, Diagnostic, maintenance and test equipment, Measurement of time, velocity, acceleration, angular velocity, Road vehicle systems, Power transmission and distribution networks, Wind turbine systems and other alternative sources of energy, Agricultural machines, implements and equipment, Transport, Elements of buildings, Construction materials, Air quality, Aerosol containers.


Military Standard of the People's Republic of China-General Armament Department, wind tunnel

  • GJB 1179A-2012 Requirement for flow quality of low and high speed wind tunnels
  • GJB 1179-1991 High-speed wind tunnel and low-speed wind tunnel flow field quality specifications
  • GJB 4017A-2021 Wind tunnel test code
  • GJB 4017-2000 Wind tunnel test code
  • GJB 2244A-2011 Specification for wind tunnel strain gage balance
  • GJB 2244-1994 Specification for wind tunnel strain balances
  • GJB 6756-2009 Test rules for low density wind tunnel
  • GJB 4296-2001 Wind tunnel testing terminology and symbols
  • GJB 7341-2011 Aerodynamic test method in shock tunnel
  • GJB 7902-2012 Test method for aerodynamic pressure measurement in high speed wind tunnel
  • GJB 2985A-2009 Design standard for shock tunnel models
  • GJB 3477-1998 Shock tunnel flow field quality requirements
  • GJB 569-1988 High-speed wind tunnel model design specifications
  • GJB 2985-1997 Shock tunnel model design criteria
  • GJB 5817-2006 Wind tunnel test requirements of minitype wind powered generator
  • GJB 180A-2006 Design criteria of aircraft test model in low speed wind tunnel
  • GJB 6757-2009 Test method of launch vehicle in low speed wind tunnel
  • GJB 2987-1997 Hypersonic wind tunnel model design criteria
  • GJB 180-1986 Design specifications for low-speed wind tunnel aircraft models
  • GJB 4232-2001 Design criteria for piezoelectric balances in shock wave wind tunnels
  • GJB 6611-2008 Test method of helicopter rotor model in low speed wind tunnel
  • GJB 5221-2004 Wind tunnel control system design and calibration criteria
  • GJB 5224-2004 Wind tunnel measurement system design and calibration criteria
  • GJB 5202-2003 General requirements for helicopter rotor wind tunnel testing
  • GJB 4399-2002 Hypersonic wind tunnel aerodynamic test method
  • GJB 5816-2006 Operation rules of high frequency inductive coupled plasma wind tunnel
  • GJB 6758-2009 Test method of pressure measurement in conventional hypersonic wind tunnel
  • GJB 8217-2014 Test method for vehicle inlet in high speed wind tunnel
  • GJB 8216-2014 Test method for aircraft inlet in low speed wind tunnels
  • GJB 8459-2015 Test method for aerodynamic measurement on air vehicle half model in high speed wind tunnel
  • GJB 8458-2015 Test method for aerodynamic measurement on air vehicle half model in low speed wind tunnel
  • GJB 7051-2010 Design criterion for wind tunnel strain gauge pressure transducer/sensor
  • GJB 5816A-2021 High frequency induction heating wind tunnel test operating procedures
  • GJB 6612-2008 Test method for aerodynamic force measurements in hypersonic low density wind tunnel
  • GJB 6755-2009 Test method for jettison of airborne external stores in low speed wind tunnel
  • GJB 4395A-2021 Aerospace vehicle low-speed wind tunnel force measurement test method
  • GJB 2986-1997 Design criteria for hypersonic low-density wind tunnel models
  • GJB 4008-2000 High-speed wind tunnel load test procedures for aircraft external stores
  • GJB 5314-2004 Low-speed wind tunnel pressure test method for aerospace vehicles
  • GJB 9997-2021 High-speed wind tunnel test method for aircraft model jets
  • GJB 6379-2008 Test methods of optical flow visualization in hypersonic wind tunnel
  • GJB 4012A-2021 Hypersonic wind tunnel cold/hot spray test model design criteria
  • GJB 2986A-2020 Design criteria for hypersonic low-density wind tunnel test model
  • GJB 2987-1997(XG1-2015) Hypersonic Wind Tunnel Model Design Guidelines Modification Sheet 1-2015
  • GJB 4297-2001 Wind tunnel force measurement, pressure measurement and thermal test information collection requirements
  • GJB 6753-2009 Test method for powered model of propeller driven aircraft in low speed wind tunnel
  • GJB 8461-2015 Test method for hinge moment measurement of air vehicle control surface in high speed wind tunnel
  • GJB 8460-2015 Test method for hinge moment measurement of air vehicle control surface in low speed wind tunnel
  • GJB 4399-2002(XG1-2015) Hypersonic wind tunnel aerodynamic test method revision sheet 1-2015
  • GJB 4990-2003 Low speed and high angle of attack wind tunnel test methods for aerospace vehicles
  • GJB 7347-2011 Blunt wedge test method for thermal-protection materials of space vehicle in arc-heated wind tunnel
  • GJB 3480-1998 Low-speed wind tunnel test method for aircraft model rotation and oscillation motion
  • GJB 3480A-2021 Low-speed wind tunnel test method for aircraft model rotation and oscillation motion
  • GJB 4012-2000 Design criteria for cold/hot jet model of hypersonic propulsion wind tunnel missile
  • GJB 4008-2000(XG1-2015) Modification sheet for high-speed wind tunnel force testing procedures for aircraft external stores 1-2015
  • GJB 6755-2009(XG1-2015) Modification sheet 1-2015 for the low-speed wind tunnel test method for airborne external stores
  • GJB 8084-2013 Stage separation test method of missile/launch vehicle model in hypersonic wind tunnel
  • GJB 6753-2009(XG1-2015) Revision sheet 1-2015 of low-speed wind tunnel test method for powered model of propeller aircraft

未注明发布机构, wind tunnel

  • GJB 1061-1991 Accuracy index of high-speed wind tunnel and low-speed wind tunnel force measurement experiments
  • GJB 569A-2012 High speed wind tunnel model design criteria
  • GJB 4395-2002 Aerospace vehicle low-speed wind tunnel force measurement test method
  • GJB 7658-2012 High-speed wind tunnel test method for full model force measurement of aircraft

Professional Standard - Aviation, wind tunnel

  • HB 7606-1998 Wind Tunnel Energy Saving Monitoring
  • HB 6758-1993 General requirements for low-velocity wind tunnel launch test of suspended objects
  • HB 8582-2020 Requirements of pressure measuring test for airfoil aerodynamic performance in the low speed wind tunnel
  • HB 8599-2021 Installation requirements for aircraft low-speed pressurized wind tunnel high Reynolds number test model
  • HB 8601-2021 Full model design requirements for aircraft low-speed pressurized wind tunnel high Reynolds number tests
  • HB 8598-2021 Design requirements for semi-model of aircraft low-speed pressurized wind tunnel high Reynolds number test
  • HB 8600-2021 General requirements for stress calculation of aircraft low-speed pressurized wind tunnel high Reynolds number test model

Group Standards of the People's Republic of China, wind tunnel

  • T/CSAE 146-2020 Full scale automotive aerodynamic wind tunnel test—The method of automotive aerodynamic performance test
  • T/ZZB 0885-2018 Supersonic pneumatic control valve
  • T/CEC 559-2021 Standard for wind tunnel test methods for overhead transmission lines
  • T/CSAE 113-2019 Wind noise test for full—Scale automobile in aero-acoustical wind tunnel—The measurement method of interior wind noise
  • T/CSAE 147-2020 Wind noise test for fullscale automobile in aero-acoustical wind tunnel—The measurement method of leakage noise
  • T/CSAE 114-2019 Automotive powertrain cooling test method in climatic wind tunnel

Society of Automotive Engineers (SAE), wind tunnel

ESDU - Engineering Sciences Data Unit, wind tunnel

  • DWN 11006-2011 Extrapolating Wind-Tunnel Data (Issue 2)
  • ESDU 90005 B-1991 Frequencies of resonance in wind tunnels with ventilated walls and plenum chamber.
  • ESDU 05022-2006 Extrapolating wind-tunnel data to full-scale Reynolds number. Part 1: Principles
  • ESDU 07010-2007 Extrapolating wind-tunnel data to full-scale Reynolds number Part 2: Procedures
  • ESDU 76028 A-1995 Lift-interference and blockage corrections for two-dimensional subsonic flow in ventilated and closed wind-tunnels.
  • ESDU 95014-1995 Upwash interference for wings in solid-liner wind tunnels using subsonic linearised-theory.

National Aeronautics and Space Administration (NASA), wind tunnel

  • NASA NACA-TM-1122-1947 Systematic Wind-Tunnel Measurements on Missiles
  • NASA NACA-TN-419-1932 Wind-tunnel tests of the Fowler variable-area wing
  • NASA NACA-TM-1095-1946 Wind-Tunnel Investigation of the Horizontal Motion of a Wing Near the Ground
  • NASA NACA-TN-705-1939 Wind-tunnel investigation of ground effect on wings with flaps
  • NASA NACA-TN-775-1940 Analysis of wind-tunnel data on directional stability and control
  • NASA-TM-78650-1978 Wind-tunnel results for an improved 21-percent-thick low-speed airfoil section
  • NASA-TP-1919-1981 Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section
  • NASA NACA-ACR-L5H08-1945 Supersonic-tunnel tests of projectiles in Germany and Italy
  • NASA NACA-TN-3497-1955 Summary of results of a wind-tunnel investigation of nine related horizontal tails
  • NASA-NGR-17-002-043-1968 Wind tunnel investigations of vortex breakdown on slender sharp edged wings
  • NASA NACA-ACR-3I20-1943 Wind-Tunnel Investigation of a Low-Drag Airfoil Section with a Double Slotted Flap
  • NASA NACA-ACR-3L08-1943 Wind-tunnel data on the aerodynamic characteristics of airplane control surfaces
  • NASA NACA-ARR-3E25-1943 Full-scale tunnel investigation of the pressure distribution over the tail of the P-47B airplane
  • NASA NACA-RM-A7L16-1948 A WIND-TUNNEL INVESTIGATION AT LOW SPEED OF VARIOUS LATERAL CONTROLS ON A 45° SWEPT-BACK WING
  • NASA NACA-WR-L-628-1944 Tests of the Northrop MX-334 glider airplane in the NACA full-scale tunnel
  • NASA NACA-TR-781-1944 Wind-tunnel procedure for determination of critical stability and control characteristics of airplanes
  • NASA NACA-ARR-3L10-1943 Wind-tunnel investigation of an NACA 23012 airfoil with a 0.30-airfoil-chord double slotted flap
  • NASA NACA-ARR-L4J05-1944 Wind-tunnel investigation of an NACA 23021 airfoil with a 0.32-airfoil-chord double slotted flap
  • NASA NACA-TN-755-1940 Wind-tunnel investigation of an N.A.C.A. 23030 airfoil with various arrangements of slotted flaps
  • NASA NACA-TN-763-1940 Wind-tunnel investigation of two airfoils with 25-percent-chord Gwinn and plain flaps
  • NASA NACA-TR-664-1939 Wind-Tunnel Investigation of an N.A.C.A. 23012 Airfoil with Various Arrangements of Slotted Flaps
  • NASA NACA-RM-L8K22-1949 Two-dimensional wind-tunnel investigation of two NACA 6-series airfoils with leading-edge slats
  • NASA-TM-4061-1988 Wind tunnel wall interference (January 1980-May 1988): A selected, annotated bibliography
  • NASA NACA-ACR-4B28-1944 Wind-tunnel investigation of control-surface characteristics XVIII - a linked overhang aerodynamic balance
  • NASA NACA-TN-715-1939 Wind-tunnel investigation of an N.A.C.A. 23012 airfoil with two arrangements of a wide-chord slotted flap
  • NASA NACA-TN-3176-1954 Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds
  • NASA NACA-TR-723-1941 Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils equipped with 40-percent-chord double slotted flaps
  • NASA NACA-WR-L-454-1942 Wind-tunnel investigation of control-surface characteristics VI - a 30-percent-chord plain flap on the NACA 0015 airfoil
  • NASA NACA-TR-661-1939 Tests in the variable-density wind tunnel of the N.A.C.A. 23012 airfoil with plain and split flaps
  • NASA NACA-TR-668-1939 Wind-tunnel investigation of N.A.C.A. 23012, 23021, and 23030 airfoils with various sizes of split flap
  • NASA-TR-D-747-1942 Wind-tunnel tests of four - and six-blade single - and dual-rotating tractor propellers
  • NASA NACA-RM-L7A30-1947 Wind-tunnel investigation of air loads over a double slotted flap on the NACA 65(216)-215, a = 0.8 airfoil section
  • NASA NACA-RM-L7D11-1947 Wind-tunnel investigation of bomb-bay configurations intended to minimize the tumbling of light-weight bombs
  • NASA NACA-TN-808-1941 Wind-tunnel investigation of an NACA 23012 airfoil with several arrangements of slotted flaps with extended lips
  • NASA NACA-TN-1545-1948 Wind-tunnel investigation of seven thin NACA airfoil sections to determine optimum double-slotted-flap configurations
  • NASA NACA-WR-L-489-1940 Drag analysis of single-engine military airplanes tested in the NACA full-scale wind tunnel
  • NASA-TN-D-5364-1969 Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap
  • NASA NACA-RM-L7K06-1948 Two-dimensional wind-tunnel investigation at high Reynolds numbers of an NACA 65A006 airfoil with high-lift devices
  • NASA NACA-RM-L8D29-1948 Wind-tunnel investigation of high-lift and stall-control devices on a 37 degrees sweptback wing of aspect ratio 6 at high Reynolds numbers
  • NASA NACA-RM-L57H13-1957 BUFFET TESTS OF AN ATTACK-AIRPLANE MODEL WITH EMPHASIS ON ANALYSIS OF DATA FROM WIND-TUNNEL TESTS
  • NASA NACA-TN-702-1936 Wind-tunnel tests of several forms of fixed wing slot in combination with a slotted flap on an N.A.C.A. 23012 airfoil
  • NASA NACA-TN-1473-1947 High-speed wind-tunnel investigation of high lift and aileron-control characteristics of an NACA 65-210 semi-span wing
  • NASA-TN-D-4664-1968 Wind-tunnel study to explore the use of slot spoilers to modulate the flap-induced lift of a wing
  • NASA-TN-D-4983-1969 Full-scale wind-tunnel investigation of static longtudinal and lateral characteristics of a light twin-engine airplane
  • NASA-TN-D-8260-1976 A design approach and selected wind tunnel results at high subsonic speeds for wing-tip mounted winglets
  • NASA NACA-ACR-4C11-1944 Wind-Tunnel Investigation of Shielded Horn Balances and Tabs on a 0.7-Scale Model of XF6F Vertical Tail Surface
  • NASA NACA-RM-L53J21-1953 Wind-tunnel investigation at transonic speeds of a spoiler-slot-deflector combination on an unswept NACA 65A006 wing
  • NASA NACA-TN-1277-1947 Two-dimensional wind-tunnel investigation of the NACA 64(sub 1)-012 airfoil equipped with two types of leading-edge flap
  • NASA NACA-TR-825-1945 Analysis of wind-tunnel stability and control tests in terms of flying qualities of full-scale airplanes
  • NASA-TP-2772-1987 Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing
  • NASA-TM-81745-1981 Low and high speed propellers for general aviation - Performance potential and recent wind tunnel test results
  • NASA NACA-RM-L55F21-1955 Wind-tunnel investigation at low speed of sideslipping, rolling, yawing, and pitching characteristics for a model of a 45 degrees swept-wing fighter-type airplane
  • NASA NACA-TN-1766-1948 Wind-tunnel investigation of effects of tail length on the longitudinal and lateral stability characteristics of a single-propeller airplane model
  • NASA-TN-D-3797-1967 Large-scale wind tunnel tests of a subsonic transport with AFT engine nacelles and high tail
  • NASA NACA-ARR-3F29-1943 Wind-tunnel investigation of control-surface characteristics XIV - NACA 0009 airfoil with a 20-percent-chord double plain flap
  • NASA NACA-TN-1417-1947 High-speed wind-tunnel tests of an NACA 0009-64 airfoil having a 33.4-percent-chord flap with an overhang 20.1 percent of the flap chord
  • NASA-TN-D-6058-1970 Wind-tunnel investigation of a jet transport airplane configuration with high thrust-weight ratio and an external-flow jet flap
  • NASA-TN-D-7721-1974 Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack
  • NASA-TM-X-311-1960 A wind-tunnel investigation of the aerodynamic characteristics of bodies of revolution at mach numbers of 2.37, 2.98, and 3.90 at angles of attack to 90 deg
  • NASA NACA-ACR-L5F27-1945 Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section
  • NASA NACA-CB-L4G10-1944 Wind tunnel investigation of NACA 66(215)-216, 66,1-212, and 65(sub 1)-212 airfoils with 0.20-airfoil-chord split flaps
  • NASA NACA-RM-L8K19-1949 Wind-tunnel investigation at low speeds of various plug-aileron and lift-flap configurations on a 42 degrees sweptback semispan wing
  • NASA NACA-RM-A8B11-1948 Wind-tunnel investigation of horizontal tails. II - unswept and 35 degrees swept-back plan forms of aspect ratio 4.5
  • NASA NACA-ARR-L4I11 REV F-1944 Wind-Tunnel Investigation of Control-Surface Characteristics XX - Plain and Balanced Flaps on an NACA 0009 Rectangular Semispan Tail Surface
  • NASA NACA-RM-A7K24-1948 Wind-tunnel investigation of horizontal tails. I - unswept and 35 degrees swept-back plan forms of aspect ratio 3
  • NASA NACA-RM-A7L02-1948 A summary and analysis of wind-tunnel data on the lift and hinge-moment characteristics of control surfaces up to a Mach number of 0.90
  • NASA NACA-RM-A8H30-1948 Wind-tunnel investigation of horizontal tails. III - unswept and 35 degrees swept-back plan forms of aspect ratio 6
  • NASA NACA-RM-A8J21-1948 Wind-tunnel investigation of horizontal tails IV : unswept plan form of aspect ratio 2 and a two-dimensional model
  • NASA NACA-TN-1327-1947 Wind-tunnel investigation of the effect of power and flaps on the static lateral characteristics of a single-engine low-wing airplane model
  • NASA-CR-2215-1977 Two-dimensional wind-tunnel tests of a NASA supercritical airfoil with various high-lift systems Volume II - Test data
  • NASA-TN-D-4448-1968 Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios
  • NASA-TN-D-7149-1973 Wind-tunnel investigation of static longitudinal and lateral characteristics of a full-scale mockup of a light single engine high-wing airplane
  • NASA-TM-X-2313-1971 Large-scale wind-tunnel tests of a propeller-driven deflected slipstream STOL model in ground effect
  • NASA-TP-1419-1979 Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model

Professional Standard - Aerospace, wind tunnel

  • QJ 2895-1997 Gun wind tunnel heat transfer test method
  • QJ 1884-1990 General specification for wind tunnel strain balances
  • QJ 2343-1992 Classification and codes of wind tunnel test objects
  • QJ 1637-1989 General Specification for Transonic Wind Tunnel Models
  • QJ 2798-1996 Aerospace vehicle cannon wind tunnel force test method
  • QJ 1965-1990 Principles and Processing Methods of Wind Tunnel Test Data Acquisition
  • QJ 2283-1992 Hypersonic wind tunnel dynamometer standard model test specification
  • QJ 2721-1995 Aerospace Vehicle Transonic Wind Tunnel Force Test Method
  • QJ 2593-1994 Transonic wind tunnel pressure test method for aerospace vehicles
  • QJ 1916.3-1990 Aerodynamic database data element Code of major domestic wind tunnels
  • QJ 1916.4-1990 Aerodynamic database data element codes of major foreign wind tunnels
  • QJ 1964-1990 Evaluation Method of Precision and Accuracy of Wind Tunnel Dynamometer Test
  • QJ 2074-1991 Wind tunnel test method for surface-to-surface missiles and launch vehicles with ground wind loads
  • QJ 2119-1991 Application and Analysis of Transponder and Supersonic Wind Tunnel Missile Force Test Results
  • QJ 1916.6-1990 Aerodynamic database data element main wind tunnel standard model code
  • QJ 1916.7-1990 Aerodynamic database data element domestic wind tunnel model test type code
  • QJ 1916.8-1990 Aerodynamic database data element wind tunnel test model aerodynamic component code
  • QJ 1916.10-1990 Aerodynamic database data element wind tunnel test force measurement data acquisition card and filling specification
  • QJ 1916.11-1990 Aerodynamic database data element wind tunnel test pressure measurement data acquisition card and filling specifications

GB-REG, wind tunnel

AIAA - American Institute of Aeronautics and Astronautics, wind tunnel

  • S-071-1995 Assessment of Wind Tunnel Data Uncertainty
  • R-092-1-2003 Wind Tunnel Testing Part 1: Management Volume
  • R-093-2003 Calibration of Subsonic and Transonic Wind Tunnels
  • R-092-2-2003 Wind Tunnel Testing Part 2: Practitioners Volume
  • G-129-2012 Nomenclature and Axis Systems for Aerodynamic Wind Tunnel Testing
  • S-071A-1999 Assessment of Experimental Uncertainty with Application to Wind Tunnel Testing
  • R-091-2003 Calibration and Use of Internal Strain- Gage Balances with Application to Wind Tunnel Testing

National Metrological Verification Regulations of the People's Republic of China, wind tunnel

  • JJG 02-1997 Mining low-speed wind tunnel verification regulations

中国气象局, wind tunnel

  • QX/T 323-2016 Meteorological low-speed wind tunnel technical conditions

American Institute of Aeronautics and Astronautics (AIAA), wind tunnel

  • AIAA R-092-1-2003 Wind Tunnel Testing Part 1: Management Volume
  • AIAA R-092-2-2003 Wind Tunnel Testing Part 2: Practitioners Volume
  • AIAA S-071A-1999 Assessment of Experimental Uncertainty with Application to Wind Tunnel Testing
  • AIAA G-129-2012 Nomenclature and Axis Systems for Aerodynamic Wind Tunnel Testing
  • AIAA R-091-2003 Calibration and Use of Internal Strain- Gage Balances with Application to Wind Tunnel Testing

American Society of Civil Engineers (ASCE), wind tunnel

SAE - SAE International, wind tunnel

Professional Standard - Machinery, wind tunnel

  • JB/T 11798-2014 Internal combustion engines.Heat exchangers.Wind tunnel test equipments

Professional Standard - Construction Industry, wind tunnel

  • JGJ/T 338-2014 Standard for wind tunnel test of buildings and structures

API - American Petroleum Institute, wind tunnel

  • API PUBL 2558-1993 Wind Tunnel Testing of External Floating-Roof Storage Tanks (First Edition)
  • API PUBL 4402-1984 Dispersion of Emissions from Offshore Oil Platforms: A Wind-Tunnel Modeling Evaluation (Withdrawn)

Professional Standard - Meteorology, wind tunnel

  • QX/T 84-2007 Test specification for meteorological low speed wind tunnel performance

Professional Standard - Civil Aviation, wind tunnel

Professional Standard - Military and Civilian Products, wind tunnel

  • WJ 2401-1997 Supersonic Static Force Measurement by Wind Tunnel Experiment Method of Projectile and Arrow

YU-JUS, wind tunnel

  • JUS H.D8.116-1987 Electric detonators. Methods of testing permitted detonators in testing tunnel

国家市场监督管理总局、中国国家标准化管理委员会, wind tunnel

General Administration of Quality Supervision, Inspection and Quarantine of the People‘s Republic of China, wind tunnel

  • GB/T 19068.3-2003 Off-grid wind turbine generator system Part 3: Wind tunnel test methods
  • GB/T 32241-2015 Laboratory method for measuring spray drift of plant protection machinery wind tunnel test

Professional Standard-Ships, wind tunnel

  • CB/Z 20013-2012 Procedure for model test on submarine wake characteristics in low speed wind tunnel

International Organization for Standardization (ISO), wind tunnel

  • ISO 22856:2008 Equipment for crop protection - Methods for the laboratory measurement of spray drift - Wind tunnels
  • ISO 17713-1:2007 Meteorology - Wind measurements - Part 1: Wind tunnel test methods for rotating anemometer performance

British Standards Institution (BSI), wind tunnel

  • BS ISO 22856:2009 Equipment for crop protection. Methods for the laboratory measurement of spray drift. Wind tunnels
  • BS ISO 22856:2008 Equipment for crop protection - Methods for the laboratory measurement of spray drift - Wind tunnels
  • BS ISO 17713-1:2007 Meteorology. Wind measurements. Wind tunnel test methods for rotating anemometer performance

ASHRAE - American Society of Heating@ Refrigerating and Air-Conditioning Engineers@ Inc., wind tunnel

  • ASHRAE 3803-1994 Cross-Ventilation and Room Partitions: Wind Tunnel Experiments on Indoor Airflow Distribution
  • ASHRAE DA-00-14-2-2000 Investigation of Static Microisolators in Wind Tunnel Tests and Validation of CFD Cage Model

German Institute for Standardization, wind tunnel

  • DIN 81208-22:2010 Manoeuvring of ships - Part 22: Wind tunnel test; Text in German and English
  • DIN ISO 17713-1:2007 Meteorology - Wind measurements - Part 1: Wind tunnel test methods for rotating anemometer performance (ISO 17713-1:2007) English version of DIN ISO 17713-1:2007-10
  • DIN ISO 17713-1:2007-10 Meteorology - Wind measurements - Part 1: Wind tunnel test methods for rotating anemometer performance (ISO 17713-1:2007)

Danish Standards Foundation, wind tunnel

  • DS/ISO 22856:2009 Equipment for crop protection - Methods for the laboratory measurement of spray drift - Wind tunnels

American Society for Testing and Materials (ASTM), wind tunnel

  • ASTM C1569-03 Standard Test Method for Wind Resistance of Concrete and Clay Roof Tiles (Wind Tunnel Method)
  • ASTM C156-02b Standard Test Method for Water Retention by Concrete Curing Materials
  • ASTM C156-02a Standard Test Method for Water Retention by Concrete Curing Materials
  • ASTM C1569-03(2009) Standard Test Method for Wind Resistance of Concrete and Clay Roof Tiles (Wind Tunnel Method)
  • ASTM C1569-03(2016) Standard Test Method for Wind Resistance of Concrete and Clay Roof Tiles (Wind Tunnel Method)
  • ASTM C1569-22 Standard Test Method for Wind Resistance of Concrete and Clay Roof Tiles (Wind Tunnel Method)
  • ASTM E2872-14(2019) Standard Guide for Determining Cross-Section Averaged Characteristics of a Spray Using Laser-Diffraction Instruments in a Wind Tunnel Apparatus

Korean Agency for Technology and Standards (KATS), wind tunnel

  • KS I ISO 17713-1:2020 Meteorology — Wind measurements — Part 1: Wind tunnel test methods for rotating anemometer performance
  • KS I ISO 17713-1:2009 Meteorology-Wind measurements-Part 1:Wind tunnel test methods for rotating anemometer performance

KR-KS, wind tunnel

  • KS I ISO 17713-1-2020 Meteorology — Wind measurements — Part 1: Wind tunnel test methods for rotating anemometer performance

Guangdong Provincial Standard of the People's Republic of China, wind tunnel

  • DB44/T 1451-2014 Test methods for dynamic heat and moisture transfer properties of building materials and components - Wind tunnel method for hot and humid climates

Association of German Mechanical Engineers, wind tunnel

  • VDI 3783 Blatt 12-2000 Environmental meteorology - Physical modelling of flow and dispersion processes in the atmospheric boundary layer - Application of wind tunnels

GM Europe, wind tunnel

  • GME L-1B1201-2010 Linearity Test at Passenger Vehicle Heating and A/CSystems on Heater Test Bench and in the Climatic Wind Tunnel




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