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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

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

Factors affecting the maximum lift-drag ratio at high 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


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