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NACA Research Memorandums
34
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NACA Research Memorandums
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1951
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1951
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Division of Load Among the Wing, Fuselage, and Tail of Aircraft
Aerodynamic Characteristics of Wings Designed for Structural Improvement
Investigation of annular liquid flow with concurrent air flow in horizontal tubes
Limits of Flammability of Pure Hydrocarbon-Air Mixtures at Reduced Pressures and Room Temperature
Comparison of Zero-Lift Drags Determined by Flight Tests at Transonic Speeds of Symmetrically Mounted Nacelles in Various Spanwise Positions on a 45 Degrees Sweptback Wing and Body Combination
Drag interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02
Review of some recent data on buffet boundaries
Aerodynamic Characteristics of Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-Stream Mach Numbers From 1.50 to 1.99
Influence of airfoil trailing-edge angle and trailing-edge-thickness variation on the effectiveness of a plain flap at high subsonic Mach numbers
Performance characteristics of aircraft cooling ejectors having short cylindrical shrouds
Preliminary Investigation of Helmholtz Resonators for Damping Pressure Fluctuations in 3.6-Inch Ram Jet at Mach Number 1.90
Internal Flow and Burning Characteristics of 16-inch Ram Jet Operating in a Free Jet at Mach Numbers of 1.35 and 1.73
Theoretical and Experimental Investigation of Additive Drag
A comparison of the experimental and theoretical loading over triangular wings in sideslip at supersonic speeds
Analysis of experimental sea-level transient data and analog method of obtaining altitude response for turbine-propeller engine with relay-type speed control
A semi-empirical method for calculating the pitching moment of bodies of revolution at low Mach numbers
Criterions for prediction and control of ram-jet flow pulsations
Altitude-performance and Reynolds number investigation of centrifugal-flow-compressor turbojet engine
Combustion performance evaluation of magnesium-hydrocarbon slurry blends in a simulated tail-pipe burner
Note on flutter of a 60 degree delta wing encountered at low-supersonic speeds during the flight of a rocket-propelled model
Notes on Heat-Resistant Materials in Britain from Technical Mission October 13 to November 30, 1950
Preliminary Results of a Flight Investigation of 1/6-Scale Rocket-Powered Models of the Bell MX-776 to Determine Aileron Rolling Effectiveness and Total Drag
Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of a canard missile configuration
Theoretical performance of lithium and fluorine as a rocket propellant
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