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Technical Report Archive and Image Library
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Technical Report Archive and Image Library
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NACA Research Memorandums
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Trace elements memorandum report
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1953
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1953
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Technical Report Archive and Image Library
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Transformation and Magnetic Phenomena Occuring in Boron Stainless Steel Vertical Safety Rods
Theoretical Performance of Liquid Hydrogen and Liquid Fluorine as a Rocket Propellant
The Effect of Blade-Section Camber on the Stall-Flutter Characteristics of Three NACA Propellers at Zero Advance
Preliminary Results of Heat Transfer from a Stationary and Rotating Ellipsoidal Spinner
Effect of Fuel Injectors and Liner Design on Performance of an Annular Turbojet Combustor With Vapor Fuel
Low-speed wind-tunnel investigation of a thin 60 degree delta wing with double slotted, single slotted, plain, and split flaps
Altitude Wind Tunnel Investigation of the Prototype J40-WE-8 Turbojet Engine Without Afterburner
Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant
Investigation of Effects of Grain Size Upon Engine Life of Cast AMS 5385 Gas Turbine Blades
Investigation of 16-inch impulse-type supersonic compressor rotor with turning past axial direction
Static Longitudinal Stability and Control Characteristics of a 1/16 -Scale Model of the Douglas D-558-II Research Airplane at Mach Numbers of 1.61 and 2.01
Flight Investigation at Mach Numbers From 0.67 to 1.81 of the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-Wing Missile Configuration Having an All-Movable Tail
Effect of fuel injectors and liner design on performance of an annular turbojet combustor with vapor fuel
Investigation of Pressure Recovery of a Single-Conical-Shock Nose Inlet at Mach Number 5.4
Experimental and theoretical study of the interference at low speed between slender bodies and triangular wings
A Transonic Wind-Tunnel Investigation of an Unswept-Wing-Body Combination at Angles of Attack Up to 24 Degrees
Air-flow and thrust characteristics of several cylindrical cooling-air ejectors with a primary to secondary temperature ratio of 1.0
The effect at high subsonic speeds of a flap-type aileron on the chordwise pressure distribution near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil section
Performance Characteristics of a 24 Degree Straight-Outer-Wall Annular-Diffuser-Tailpipe Combination Utilizing Rectangular Vortex Generators for Flow Control
Free-Spinning-Tunnel Investigation to Determine the Effect on Spins and Recoveries of Wing Leading-Edge Chord-Extensions and Drooped Leading-Edge Flaps on Scale Models of Two Sweptback-Wing Fighter Airplanes
The Design of Brittle-Material Blade Roots Based on Theory and Rupture Tests of Plastic Models
Pressure and Force Characteristics at Transonic Speeds of a Submerged Divergent-Walled Air Inlet on a Body of Revolution
Altitude Starting Characteristics of an Afterburner With Autoignition and Hot-Streak Ignition
Flight Measurements of the Horizontal-Tail Loads on a Swept-Wing Fighter Airplane at Transonic Speeds
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