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The Time Lag Between Flap Deflection and Force Development at a Mach Number of 4
Results Obtained During Flights 1 to 6 of the Northrop X-4 Airplane (A.F. No. 46-677)
Pressure-Rise and Leakage-Loss Characteristics of a Rotating Cowling
Effects of Obstructions in Compressor Inlet on Blade Vibration in 10-Stage Axial-Flow Compressor
Ditching Tests With a 1/16-Size Model of the Navy XP2V-1 Airplane at the Langley Tank No. 2 Monorail
Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane
The Calculation of the Path of a Jettisonable Nose Section
Ability of Pilots to Control Simulated Short-Period Yawing Oscillations
Maximum-Lift Investigation of a 1/40-Scale X-1 Airplane Wing at Mach Numbers From 0.60 to 1.15