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NACA Research Memorandums
158
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Preliminary performance data of several tail-pipe-cascade-type model thrust reversers
An experimental investigation of two methods for reducing transonic drag of swept-wing and body combinations
Experimental investigation of methods of improving diffuser-exit total-pressure profiles for side-inlet model at Mach number 3.05
Aerodynamic Characteristics of a 1/4-Scale Model of the Duct System for the General Electric P-1 Nuclear Powerplant for Aircraft
Experimental study of shock-positioning method of ram-jet-engine control
Experimental investigation of drag of afterbodies with exiting jet at high subsonic Mach numbers
Stability and Control Characteristics at High Subsonic Speeds of a 1/30-Scale Model of the MX-1554A Design
Theoretical Performance of Mixtures of Liquid Ammonia and Hydrazine as Fuel With Liquid Fluorine as Oxidant for Rocket Engines
Effects of a Straightening Operation on Performance of Inconel 550 Buckets
Factors affecting flow distortions produced by supersonic inlets
Design of Combustor for Long-Range Ram-Jet Engine and Performance of Rectangular Analog
Preliminary Transient Performance Data on the Fuel Control of the XRJ47-W-5 Ram-Jet Engine
Component and over-all performance evaluation of a J47-GE-25 turbojet engine over a range of engine-inlet Reynolds number indices
Flight Investigation to Evaluate the Roll-Rate Stabilization System of the Naval Ordnance Test Station SIDEWINDER Missile at Mach Numbers From 0.9 to 2.3
Heat-Transfer and Pressure Measurements From a Flight Test of the Second 1/18-Scale Model of the Titan Intercontinental Ballistic Missile Up to a Mach Number of 3.91 and Reynolds Number Per Foot of 23.4 by 10 to the 6th Power
Some Notes on the Probable Damage to an Intercontinental-Ballistic-Missile Warhead Following Puncture of the Heat Shield
Thermal Stability of Decaborane and of a Commercial Ethyl Decaborane (HEF-3) in the Range 202 Degrees to 252 Degrees C
Procedure for Measuring Liquid-Water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method
Investigation of an on-off inlet shock-position control on a 16-inch ram-jet engine
Rocket-Model Investigation of the Longitudinal Stability, Drag, and Duct Performance of a 60 Degree Delta-Wing Canard Aircraft With Twin Side Inlets at Mach Numbers From 0.80 to 1.70
High-Altitude Performance of J71-A-11 Turbojet Engine and Its Components Using JP-4 and Gaseous-Hydrogen Fuels
Calculation of External-Store Loads and Correlation With Experiment
A Study of Skin Temperatures of Conical Bodies in Supersonic Flight
An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback: Static longitudinal stability and control characteristics at a Mach number of 1.59
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