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National Advisory Committee for Aeronautics Collection
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Preliminary Investigation of the Total-Pressure-Recovery Characteristics of a 15 Degree Semiangle Movable-Cone Variable-Geometry Ram-Jet Inlet at Free-Jet Mach Numbers of 1.62, 2.00, 2.53, and 3.05
Effects of internal corner fillets on pressure recovery: Mass flow characteristics of scoop-type conical supersonic inlets
Lateral Stability and Control Measurements of a 0.0858-Scale Model of the Lockheed XF-104 Airplane at Transonic Speeds
Free-Flight Tests of 1/9-Scale Convair YF-102 Airplane Wings at Transonic and Supersonic Speeds to Investigate the Possibility of Flutter
A Transonic Wind-Tunnel Investigation of the Longitudinal Aerodynamic Characteristics of a Model of the Lockheed XF-104 Airplane
Flight Determination of Drag of Normal-Shock Nose Inlets With Various Cowling Profiles at Mach Numbers From 0.9 to 1.5
Lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds
Hydrodynamic Investigation of the the Take-Off Characteristics of a 1/10-Scale Dynamic Model of the Convair XF2Y-1 Airplane
Wind-Tunnel Investigation of the Republic F-105 Inlet with Various Modifications at Mach Numbers 1.41, 1.81, and 2.01
Factors Affecting the Starting Characteristics of Gas-Turbine Engines
A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70
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