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Investigation of an NACA Submerged Inlet at Mach Numbers from 1.17 to 1.99
An Investigation at Subsonic Speeds of the Rolling Effectiveness of a Small Perforated Spoiler on a Wing Having 45 Degrees of Sweepback
Investigation of the Effect of Sweep on the Flutter of Cantilever Wings
Low-Speed Cascade Tests of Two 45 Degree Swept Compressor Blades With Constant Spanwise Loading
Experimental Investigation of Water Injection in Subsonic Diffuser of a Conical Inlet Operation at Free-Stream Mach Number of 2.5
Stability and control characteristics of a free-flying model with an unswept wing of aspect ratio 3 (XS-3)
A Transonic Wind-Tunnel Investigation of the Aerodynamic Characteristics of Three 4-Percent-Thick Wings of Sweepback Angles 10.8 Degrees, 35 Degrees, and 47 Degrees, Aspect Ratio 3.5, and Taper Ratio 0.2 in Combination With a Body
Full-scale performance study of a prototype crash-fire protection system for reciprocating-engine-powered airplanes
Effect of Fuselage Interference on the Damping in Roll of Delta Wings of Aspect Ratio 4 in the Mach Number Range Between 0.6 and 1.6 as Determined With Rocket Propelled Vehicles
A Free-Flight Investigation at Zero Lift in the Mach Number Range Between 0.7 and 1.4 to Determine the Effectiveness of an Inset Tab as a Means of Aerodynamically Relieving Aileron Hinge Moments
Experimental investigation of a flat plate paddle jet vane operating on a rocket jet
Experimental ablation cooling
Performance of an Isentropic, All-Internal-Contraction, Axisymmetric Inlet Designed for Mach 2.50
Investigation of a Shrouded and an Unshrouded Axial-Flow Supersonic Compressor
Some internal-flow characteristics of several axisymmetrical NACA 1-series nose air inlets at zero flight speed
Investigation of a 10-Stage Subsonic Axial-Flow Research Compressor 5: Effect of Reducing Inlet-Guide-Vane Turning on Over-All and Inlet-Stage Performance
A Transonic Wind-Tunnel Investigation of the Longitudinal Force and Moment Characteristics of a Plane and a Cambered 3-Percent-Thick Delta Wing of Aspect Ratio 3 on a Slender Body
Altitude-Wind-Tunnel Investigation of Combustion-Chamber Performance on J47 Turbojet Engine
Tabulated Pressure Coefficient Data from a Tail Loads Investigation on a 1/15-Scale Model of the Goodyear XZP5K Airship
An Investigation of the Hydrodynamic Characteristics of a Jet-Powered Dynamic Model of the DR 56 Flying Boat: TED No. NACA DE 328
An Experimental Investigation of Four Triangular-Wing-Body Combinations in Sideslip at Mach Numbers 0.6, 0.9, 1.4, and 1.7
Effects of Components and Various Modifications on the Drag and the Static Stability and Control Characteristics of a 42 Deg Swept-Wing Fighter-Airplane Model at Mach Numbers of 1.60 to 2.50
Zero-Lift Drag of the Chance Vought Regulus II Missile at Mach Numbers Between 0.8 and 2.2 as Determined From the Flight Tests of Two 0.12-Scale Models
Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers 1: shock diffuser with triple-shock projecting cone
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