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Lift, drag, and static longitudinal stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28
Flight measurements of horizontal tail loads on a typical propeller-driven pursuit airplane during stalled pull-outs at high speed
Wind-Tunnel Measurements at Subsonic Speeds of the Static and Dynamic-Rotary Stability Derivatives of a Triangular-Wing Airplane Model Having a Triangular Vertical Tail
Model Ditching Investigations of Three Airplanes Equipped With Hydro-Skis
Flight Observations of Aileron Flutter at High Mach Numbers as Affected by Several Modifications
The Effect of Spanwise Aileron Location on the Rolling Effectiveness of Wings With 0 Degree and 45 Degree Sweep at Subsonic, Transonic, and Supersonic Speeds
Effects of Compressibility on the Characteristics of Five Airfoils
Investigations of an Annular Diffuser-Fan Combination Handling Rotating Flow
Experimental investigation of the drag of 30 degree, 60 degree, and 90 degree cone cylinders at Mach numbers between 1.5 and 8.2
The effect of bluntness on the drag of spherical-tipped truncated cones of fineness ratio 3 at Mach numbers 1.2 to 7.4
The Ames supersonic free-flight wind tunnel
Preliminary Data on the Effect of Body-Nose Bluntness on the Drag and Pressure Recovery of a Side-Inlet-Body Combination at Mach Numbers of 1.4 and 1.7
Model ditching investigations of three airplanes equipped with hydro-skis
The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65
General algebraic method applied to control analysis of complex engine types
Aerodynamic characteristics of a 60 degree delta wing having a half-delta tip control at a Mach number of 4.04
Lift, drag, and longitudinal stability at Mach numbers from 0.8 to 2.1 of a rocket-powered model having a tapered unswept wing of aspect ratio 3 and inline tail surfaces
Analysis of cooling-air requirements of corrugated-insert-type turbine blades suitable for a supersonic turbojet engine
Performance of supersonic ramp-type side inlet with combinations of fuselage and inlet throat boundary-layer removal
Analytical investigation of factors affecting the performance of single-stage turbines having rotor-tip discharge of cooling air
Design of two transpiration-cooled strut-supported turbine rotor blades
Temperature-control study of turbine region of turbojet engine, including turbine-blade time constants and starting characteristics
The Ames Supersonic Free-Flight Wind Tunnel
Low-Speed Wind-Tunnel Investigation of the Drag of a Lockheed F-94C Airplane (A.F. No. 50-956)
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