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large low speed wind tunnel
large low speed wind tunnel, Total:69 items.
In the international standard classification, large low speed wind tunnel involves: Geology. Meteorology. Hydrology, Aircraft and space vehicles in general, Wind turbine systems and other alternative sources of energy, Integrated circuits. Microelectronics.
Military Standard of the People's Republic of China-General Armament Department, large low speed 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 180A-2006 Design criteria of aircraft test model in low speed wind tunnel
- GJB 180-1986 Design specifications for low-speed wind tunnel aircraft models
- GJB 8458-2015 Test method for aerodynamic measurement on air vehicle half model in low speed wind tunnel
- GJB 2986-1997 Design criteria for hypersonic low-density wind tunnel models
- GJB 4990-2003 Low speed and high angle of attack wind tunnel test methods for aerospace vehicles
- GJB 2986A-2020 Design criteria for hypersonic low-density wind tunnel test model
- GJB 6757-2009 Test method of launch vehicle in low speed wind tunnel
- GJB 6753-2009 Test method for powered model of propeller driven aircraft in low speed wind tunnel
- GJB 569-1988 High-speed wind tunnel model design specifications
- GJB 6611-2008 Test method of helicopter rotor model in low speed 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 8216-2014 Test method for aircraft inlet in low speed wind tunnels
- GJB 2987-1997 Hypersonic wind tunnel model design criteria
- 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 5314-2004 Low-speed wind tunnel pressure test method for aerospace vehicles
- GJB 8459-2015 Test method for aerodynamic measurement on air vehicle half model in high speed wind tunnel
- GJB 6753-2009(XG1-2015) Revision sheet 1-2015 of low-speed wind tunnel test method for powered model of propeller aircraft
- GJB 9997-2021 High-speed wind tunnel test method for aircraft model jets
- GJB 8460-2015 Test method for hinge moment measurement of air vehicle control surface in low speed wind tunnel
- GJB 4012A-2021 Hypersonic wind tunnel cold/hot spray test model design criteria
- GJB 2987-1997(XG1-2015) Hypersonic Wind Tunnel Model Design Guidelines Modification Sheet 1-2015
- GJB 6755-2009(XG1-2015) Modification sheet 1-2015 for the low-speed wind tunnel test method for airborne external stores
- GJB 4012-2000 Design criteria for cold/hot jet model of hypersonic propulsion wind tunnel missile
- GJB 8084-2013 Stage separation test method of missile/launch vehicle model in hypersonic wind tunnel
未注明发布机构, large low speed 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-Ships, large low speed wind tunnel
- CB/Z 20013-2012 Procedure for model test on submarine wake characteristics in low speed wind tunnel
National Metrological Verification Regulations of the People's Republic of China, large low speed wind tunnel
- JJG 02-1997 Mining low-speed wind tunnel verification regulations
中国气象局, large low speed wind tunnel
- QX/T 323-2016 Meteorological low-speed wind tunnel technical conditions
National Aeronautics and Space Administration (NASA), large low speed wind tunnel
- 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-RM-A7L16-1948 A WIND-TUNNEL INVESTIGATION AT LOW SPEED OF VARIOUS LATERAL CONTROLS ON A 45° SWEPT-BACK WING
- NASA-TN-D-3797-1967 Large-scale wind tunnel tests of a subsonic transport with AFT engine nacelles and high tail
- 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-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-81745-1981 Low and high speed propellers for general aviation - Performance potential and recent wind tunnel test results
- NASA-TP-1419-1979 Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model
- NASA NACA-RM-L56D03-1956 Low-speed wind-tunnel results for a thin aspect-ratio-1.85 pointed-wing-fuselage model with double slotted flaps
- NASA-TN-D-8373-1976 Low-speed wind-tunnel investigation of flight spoilers as trailing-vortex-alleviation devices on an extended-range wide-body tri-jet airplane model
- NASA NACA-RM-L52G07-1952 Wind-tunnel investigation of the low-speed static and rotary stability derivatives of a 0.13-scale model of the Douglas D-558-II airplane in the landing configuration
- 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-TN-D-4448-1968 Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios
- NASA-TM-X-2313-1971 Large-scale wind-tunnel tests of a propeller-driven deflected slipstream STOL model in ground effect
- NASA-TM-X-3166-1975 Low-speed wind-tunnel investigation of forward-located spoilers and trailing splines as trailing-vortex hazard-alleviation devices on an aspect-ratio-8 wing model
Professional Standard - Aviation, large low speed wind tunnel
- 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 6758-1993 General requirements for low-velocity wind tunnel launch test of suspended objects
- 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, large low speed wind tunnel
- T/JSQA 056-2020 Large low-speed permanent magnet type wind turbine generator
Professional Standard - Meteorology, large low speed wind tunnel
- QX/T 84-2007 Test specification for meteorological low speed wind tunnel performance
Professional Standard - Aerospace, large low speed wind tunnel
- QJ 1637-1989 General Specification for Transonic Wind Tunnel Models
- QJ 2283-1992 Hypersonic wind tunnel dynamometer standard model test specification
National Metrological Technical Specifications of the People's Republic of China, large low speed wind tunnel
- JJF 1452-2014 Program of Pattern Evaluation of Contact Anemorumbometer
- JJF 1451-2014 Program of Pattern Evaluation of Portable 3-cup Anemometer
- JJF 1450-2014 Program of Pattern Evaluation of Portable Induction Anemometer
国家能源局, large low speed wind tunnel
Professional Standard - Machinery, large low speed wind tunnel
- JB/T 9740.2-1999 Types and basic parameters for low speed wind energy conversion system
GB-REG, large low speed wind tunnel
- REG NASA-TM-X-62197-1973 Wind-tunnel investigation of a large-scale 25 degrees swept-wing jet transport model with an external blowing triple-slotted flap
Defense Logistics Agency, large low speed wind tunnel
- DLA SMD-5962-98628-1998 MICROCIRCUIT, LINEAR, DUAL, LOW NOISE, HIGH SPEED, OPERATIONAL AMPLIFIER, MONOLITHIC SILICON