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NACA Research Memorandums
34
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NACA Research Memorandums
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The effects of boundary-layer separation over bodies of revolution with conical tail flares
Experimental investigation of the simulation of atmospheric entry of ballistic missiles
In-Flight Gains Realized by Modifying a Twin Side-Inlet Induction System
In-flight gains realized by modifying a twin side-inlet induction system
An Investigation of the Control Effectiveness of Tip Ailerons and Spoilers on a Low-Aspect-Ratio Trapezoidal-Wing Airplane Model at Mach Numbers From 1.55 to 2.35
Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating Near the Free Water Surface
Surge-Inception Study in a Two-Spool Turbojet Engine, Revised
Effect of Conical and Flat Sting-Mounted Windshields on the Zero-Lift Drag of a Flare-Stabilized Bluff Body at Mach Numbers From 0.6 to 1.15
Effect of Frequency of Sideslipping Motion on the Lateral Stability Derivatives of a Typical Delta-Wing Airplane
Effect of Ground Proximity on Aerodynamic Characteristics of Two Horizontal-Attitude Jet Vertical-Take-Off-and-Landing Airplane Models
Investigation at Mach Numbers to 1.04 of Blade-Loading Characteristics of Two Full-Scale Three-Blade Supersonic Propellers Differing in Blade-Section Camber
Temperature measurements from a flight test of two wing-body combinations at 7 degree angle of attack for Mach numbers to 4.86 and Reynolds numbers to 19.2 X 10(exp 6)
Effect of Nose Shape on Subsonic Aerodynamic Characteristics of a Body of Revolution Having a Fineness Ratio of 10.94
Jet effects on base pressures of conical afterbodies at Mach 1.91 and 3.12
Rocket-Model Investigation of Hinge-Moments on a Trailing-Edge Control on a 52.5 Degree Swept Wing Between Mach Numbers of 0.70 and 1.80
Transonic Flutter Investigation of a 64 Degree Delta Wing Constructed With Spars Along Constant-Percent Chord Lines and Streamwise Ribs
The Use of Cones as Stabilizing and Control Surfaces at Hypersonic Speeds
Experimental investigation of effects of moderate sideslip on the flow fields near a 45 degree swept-wing-fuselage combination at low speed
The Frequency Content of the Control Input and Airplane Response Obtained During Service Operations of Fighter Airplanes
Local Heat Transfer to Blunt Noses at High Supersonic Speeds
Some Factors Affecting the Static Longitudinal and Directional Stability Characteristics of Supersonic Aircraft Configurations
Some Factors Affecting the Static Longitudinal and Directional Stability Characteristics of Supersonic Aircraft Configurations
Analytical Study of the Comparative Pitch-Up Behavior of Several Airplanes and Correlation With Pilot Opinion
Cascade investigation of cooling characteristics of a cast-finned air-cooled turbine blade for use in a turboprop engine
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