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- A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel
- Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift
- Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel
- Investigation of the aerodynamic characteristics of the NACA RM-10 missile (with fins) at a Mach number of 1.62 in the Langley 9-inch supersonic tunnel
- Factors affecting transition at supersonic speeds
- Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord
- Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds
- Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail
- Application of oblique-shock sensing system to ram-jet-engine flight Mach number control
- Combustion of aluminum borohydride in a supersonic wind tunnel
- Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5
- Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
- Preliminary attempts at isothermal compression of a supersonic air stream
- Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles
- Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds
- Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine
- Factors affecting the maximum lift-drag ratio at high supersonic speeds
- Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds
- Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds
- Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds
- Span loadings due to wing twist at transonic and supersonic speeds
- Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
- Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4
- Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination
- Some measurements at subsonic speeds of the aerodynamic forces and moments on two delta wings of aspect ratios 2 and 4 oscillating about the midchord
- Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds
- Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3