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National Advisory Committee for Aeronautics Collection
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Analysis of coolant flow and pressure requirements for a return-flow turbine rotor blade design using hydrogen, helium, or air as coolant
An Analysis of Vertical-Tail Loads Measured in Flight on a Swept-Wing Bomber Airplane
Bonded lead monoxide films as solid lubricants for temperatures up to 1250 degrees F
Data From Large-Scale Low-Speed Tests of Airplane Configurations With a Thin 45 Degree Swept-Wing Incorporating Several Leading-Edge Contour Modifications
The effect of lip shape on a nose-inlet installation at Mach numbers from 0 to 1.5 and a method for optimizing engine-inlet combinations
Effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces
Experimental Investigation of a Five-Stage Axial-Flow Research Compressor with Transonic Rotors in All Stages 4: Blade-Element Performance
Experimental investigation of the effects of support interference on the drag of bodies of revolution at a Mach number of 1.5
Investigation of off-design performance of shock-in-rotor type supersonic blading
Investigation of the effects of profile shape on the aerodynamic and structural characteristics of thin, two-dimensional airfoils at supersonic speeds
Investigation of the NACA 4-(5)(08)-03 and NACA 4-(10)(08)-03 two-blade propellers at forward Mach numbers to 0.725 to determine the effects of camber and compressibility on performance
Landing Characteristics in Waves of Three Dynamic Models of Flying Boats
Lift, drag, and elevator hinge moments of Handley Page control surfaces
Measurements and Predictions of Flow Conditions on a Two-Dimensional Base Separating a Mach Number 3.36 Jet and a Mach Number 1.55 Outer Stream
Optimum Lifting Bodies at High Supersonic Airspeeds
Propagation of a free flame in a turbulent gas stream
Propeller Induced Angles of Attack and Section Angles of Attack for the NACA 10-(3)(066)-03, 10-(3)(049)-03, 10-(3)(090)-03, 10-(5)(066)-03, and 10-(0)(066)-03 Propellers
Test-stand investigation of a rectangular ram-jet engine
Tests in the variable-density wind tunnel of related airfoils having the maximum camber unusually far forward
Theories of flow similitude
The Variation in Engine Power With Altitude Determined From Measurements in Flight With a Hub Dynamometer
Wind-Tunnel Investigation of the Aerodynamic Characteristics of a 0.07-Scale Model of the North American MX-770 Missile
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