In the international standard classification, rm50 involves: .
National Aeronautics and Space Administration (NASA), rm50
NASA NACA-RM-L50A04-1950 Longitudinal characteristics of two 47.7 degrees sweptback wings with aspect ratios of 5.1 and 6.0 at Reynolds numbers up to 10 x 10(exp 6)
NASA NACA-RM-A50C13-1950 Preliminary investigation of the transonic characteristics of an NACA submerged inlet
NASA NACA-RM-A50E02-1950 Pressure-distribution and ram-recovery characteristics of NACA submerged inlets at high subsonic speeds
NASA NACA-RM-A50K20-1951 Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds - plane triangular wing of aspect ratio 2 with NACA 0008-63 section
NASA NACA-RM-E50D05-1950 Experimental investigation of supersonic flow with detached shock waves for Mach numbers between 1.8 and 2.9
NASA NACA-RM-E50H23-1950 Correlation of forced-convection heat-transfer data for air flowing in smooth platinum tube with long-approach entrance at high surface and inlet-air temperatures
NASA NACA-RM-L50E26-1950 Damping in roll of rectangular wings of several aspect ratios and NACA 65A-series airfoil sections of several thickness ratios at transonic and supersonic speeds as determined with rocket-powered models
NASA NACA-RM-L50F16-1950 Low-speed aerodynamic characteristics of a series of swept wings having NACA 65A006 airfoil sections
NASA NACA-RM-L50H29-1950 Positioning investigation of single slotted flaps on a 47.7 degrees sweptback wing at Reynolds numbers of 4.0 x 10(exp 6) and 6.0 x 10(exp 6)
NASA NACA-RM-L50K06-1951 Horizontal-tail effectiveness and downwash surveys for two 47.7 degrees sweptback wing-fuselage combinations with aspect ratios of 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6)
NASA NACA-RM-L50L29-1951 Summary of spin and recovery characteristics of 12 models of flying wing and unconventional type airplanes
NASA NACA-RM-L50L04-1951 Effects of several arrangements of rectangular vortex generators on the static-pressure rise through a short 2:1 diffuser
NASA NACA-RM-A50J09 REV A-1950 Preliminary flight investigation of the dynamic longitudinal-stability characteristics of a 35 degree swept-wing airplane
NASA NACA-RM-A50K28 REV A-1951 The effects of increasing the leading-edge radius and adding forward camber on the aerodynamic characteristics of a wing with 35 degrees of sweepback