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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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NACA Research Memorandums
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Problems of performance and heating of hypersonic vehicles
Characteristics of flow over inclined bodies of revolution
An Investigation of the Free-Spinning and Recovery Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane With Alternate Nose Configurations With and Without Wing Fuel Tanks, TED No. NACA AD 395
Investigation of altitude ignition, acceleration and steady-state operation with single combustor of J47 turbojet engine
Pressure distribution over a sharp-nose body of revolution at transonic speeds by the NACA wing-flow method
Aircraft configurations developing high lift-drag ratios at high supersonic speeds
Experimental investigation of tail-pipe-burner design variables
Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms August 16, 1947 to August 20, 1947 at Clinton County Army Air Field, Ohio
Aerodynamics of Missiles Employing Wings of Very Low Aspect Ratio
Force Characteristics in the Submerged and Planing Condition of a 1/5.78-Scale Model of a Hydro-Ski-Wheel Combination for the Grumman JRF-5 Airplane
External-Store Drag Reduction at Transonic and Low Supersonic Mach Numbers by Application of Baldwin's Moment-of-Area Rule
Preliminary comparison of 17- and 75-millimeter-bore cageless cylindrical roller bearings with conventional cylindrical roller bearings at high speeds
Analysis of Off-Design Performance of a 16-Stage Axial-Flow Compressor With Various Blade Modifications
Determination of stresses in gas-turbine disks subjected to plastic flow and creep
A reevaluaion of data on atmospheric turbulence and airplane gust loads for application in spectral calculations
Effects of Surface Roughness and Extreme Cooling on Boundary-Layer Transition for 15 Degrees Cone-Cylinder in Free Flight at Mach Numbers to 7.6
Experimental Investigation of the Effect of Circumferential Inlet Flow Distortion on the Performance of a Five-Stage Axial-Flow Research Compressor with Transonic Rotors in All Stages
A variational theorem for creep with applications to plates and columns
A Review of Recent Information on Boundary-Layer Transition at Supersonic Speeds
Investigation of the effects of geometric changes in an underwing pylon suspended external store installation on the aerodynamic characteristics of a 45 degree sweptback wing at high subsonic speeds
Design considerations for mixed-flow centrifugal compressors with high weight-flow rates per unit frontal area
Design of NACA Cowlings for Radial Air-Cooled Engines
Investigation of the Trim Characteristics of a 1/20-Scale Model of the Fleetwings XBTK-1 Airplane over a Wide Range of Angles of Attack
Performance of a Two-Dimensional Cascade Inlet at a Free-Stream Mach Number of 3.05 and at Angles of Attack of -3 Degrees, 0 Degrees, 3 Degrees, and 6 Degrees
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