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Effects of free-flight rocket-model booster-adapter configurations on the aerodynamic characteristics in pitch and sideslip of a swept-wing fighter airplane model at a Mach number of 2.01
Free-flight investigation, including some effects of wing aeroelasticity, of the rolling effectiveness of an all-movable horizontal tail with differential incidence at Mach numbers from 0.6 to 1.5
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
Flight measurements of wing loads on the Convair XF-92A delta-wing airplane
Low-Speed Investigation of the Effects of Wing Tanks and Speed Brakes on the Static Stability of a Model Having a 40 Degree Swept Wing
Preliminary investigation of short two-dimensional subsonic diffusers
Analysis of cooling-air requirements of corrugated-insert-type turbine blades suitable for a supersonic turbojet engine
Flight measurements of the low-speed characteristics of a 35 degree swept-wing airplane with blowing-type boundary-layer control in the trailing-edge flaps
The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin
Analytic evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1 : Supplement I - Influence of new boric-oxide vapor-pressure data on calculated performanc
Performance of supersonic ramp-type side inlet with combinations of fuselage and inlet throat boundary-layer removal
Preliminary Report of Experimental Investigation of Ram-Jet Controls and Engine Dynamics
The Effect of External Stiffening Ribs on the Rolling Power of Ailerons on a Swept Wing
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
A summary of results obtained during flight simulation of several aircraft prototypes with variable-stability airplanes
Temperature-control study of turbine region of turbojet engine, including turbine-blade time constants and starting characteristics
De-icing and runback characteristics of three cyclic electric, external de-icing boots employing chordwise shedding
Design and experimental investigation of a single-stage turbine with a downstream stator
Pressure Measurements at Transonic and Low Supersonic Speeds on a Thin Conical Cambered Low-Aspect-Ratio Delta Wing in Combination With Basic and Indented Bodies
An experimental study of the zero-angle-of attack transonic drag associated with the vertical position of a horizontal tail at zero incidence
Compressibility Effects on a Hovering Helicopter Rotor Having an NACA 0018 Root Airfoil Tapering to an NACA 0012 Tip Airfoil
Wind-Tunnel Data on the Longitudinal and Lateral-Directional Rotary Derivatives of a Straight-Wing, Research Airplane Configuration at Mach Numbers From 2.5 to 3.5
Investigation of the Low-Speed Stability and Control Characteristics of a 1/7-Scale Model of the North American X-15 Airplane
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