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NACA Research Memorandums
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NACA Research Memorandums
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Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds
A theoretical study of the lifting efficiency at supersonic speeds of wings utilizing indirect lift induced by vertical surfaces
Wind Tunnel Investigation at Low Speed of Aerodynamic Characteristics of Army Chemical Corps Model E-112 Bomblets with Span Chord Ratio of 2 - 1
Investigation of a 1/22-Scale of the Republic F-105 Airplane in the Langley 8-Foot Transonic Tunnel: Static Longitudinal Stability and Control and Performance Characteristics at Transonic Speeds
Full-Scale Wind-Tunnel Tests of a 35 Degree Swept-Wing Fighter Airplane With a Spoiler-Slot-Deflector Lateral Control System
An Investigation of Ejection Releases of Submerged and Semisubmerged Dynamically Scaled Stores From a Simulated Bomb Bay of a Fighter-Bomber Airplane at Supersonic Speeds
Pressure Distributions and Aerodynamic Characteristics of Several Spoiler-type Controls on a Trapezoidal Wing at Mach Numbers of 1.61 and 2.01
External-stream effects on gross thrust and pumping characteristics of ejectors operating at off-design Mach numbers
Supersonic-Area-Rule Design and Rocket-Propelled Flight Investigation of a Zero-Lift Straight-Wing-Body-Nacelle Configuration Between Mach Numbers 0.8 and 1.53
Full-scale wind-tunnel tests of a 35 degree swept-wing fighter airplane with a spoiler-slot-deflector lateral control system
Light Diffusion Through High-Speed Turbulent Boundary Layers
Wind-Tunnel Investigation of a Ram-Jet Model Having a Wing and Canard Surfaces of Delta Plan Form With 70 Degrees Swept Leading Edges: Force and Moment Characteristics at Combined Angles of Pitch and Sideslip for Mach Number 2.01
Preliminary survey of compressor rotor-blade wakes and other flow phenomena with a hot-wire anemometer
Application of area suction to leading-edge and trailing-edge flaps on a 44 degree swept-wing model
Wind-tunnel tests of blowing boundary-layer control with jet pressure ratios up to 9.5 on the trailing-edge flaps of a 35 degree sweptback wing airplane
Analysis of some parameters used in correlating blowing-type boundary-layer control data
High-temperature oxidation and ignition of metals
A Low-Speed Investigation of a High-Lift Lateral-Control Device Consisting of a Spoiler-Slot-Deflector and a Trailing-Edge Flap on a Tapered 45 Degree Sweptback Wing
Investigation of unsteady flow past four NACA 6-percent-thick airfoil sections
Investigation of a 1/22-Scale Model of the Republic F-105 Airplane in the Langley 8-Foot Transonic Tunnel: Static Longitudinal Stability and Control and Performance Characteristics at Transonic Speeds
Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of plain spoilers on thin untapered wings at transonic speeds
Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds
Measurements of Boundary-Layer Transition at Low Speed on Two Bodies of Revolution in a Low-Turbulence Wind Tunnel
Flight Tests of Fifteen T-231 Gun-Launched Rocket Projectiles
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