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NACA Research Memorandums
391
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Theoretical Analysis of the Interference Effects of Several Supersonic Tunnel Walls Capable of Absorbing the Shock Caused by the Nose of a Model
Experimental Evaluation of Swirl Can Elements for Hydrogen Fuel Combustor
An Investigation of Loads on Ailerons at Transonic Speeds
Simplified procedures for estimating flap-control loads at supersonic speeds
The Unsteady Normal-Force Characteristics of Selected NACA Profiles at High Subsonic Mach Numbers
A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds
Effect of Inlet-Guide-Vane Angle on Blade Vibration and Rotating Stall of 13-Stage Axial-Flow Compressor in Turbojet Engine
Flight Determination of the Longitudinal Stability and Control Characteristics of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback
Stabilization of 50-Percent Magnesium - JP-4 Slurries With Some Aluminum Soaps of C(Sub 8) Acids
Application of Pulse Techniques to Strain Gages
Altitude Performance of a Turbojet Engine Using Pentaborane Fuel
Investigation of Flutter Characteristics of Three Low-Aspect-Ratio All-Movable Half-Span Control Surfaces at Mach Numbers From 1.49 to 2.87
Some Effects of Flow Spoilers and of Aerodynamic Balance on the Oscillating Hinge Moments for a Swept Fin-Rudder Combination in a Transonic Wind Tunnel
Performance at Mach Numbers 3.07, 1.89, and 0 of Inlets Designed for Inlet-Engine Matching Up to Mach 3
Performance of Isentropic Nose Inlets at Mach Number of 5.6
Investigation of Lithium Hydride and Magnesium as High-Temperature Internal Coolants With Several Skin Materials
Effects of Modifications to a Control Surface on a 6-Percent-Thick Unswept Wing on the Transonic Control-Surface Flutter Derivatives
A Summary of Results Obtained During Flight Simulation of Several Aircraft Prototypes With Variable-Stability Airplanes
A Feasibility Study of the Flare-Cylinder Configuration as a Reentry Body Shape for an Intermediate Range Ballistic Missile
The Effect of Blunt-Trailing-Edge Modifications on the High-Speed Stability and Control Characteristics of a Swept-Wing Fighter Airplane
Analysis of pressure distributions for a series of tip and trailing-edge controls on a 60 deg wing at Mach numbers of 1.61 and 2.01
Investigation of the possibility of simplifying missile guidance systems by the use of free-floating flaps and spring-mounted control surfaces
Experimental investigation of deposition by boron-containing fuels in turbojet combustor
NACA Investigations of Icing-Protection Systems for Turbojet-Engine Installations
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