348 Matching Results

This system will be undergoing maintenance January 22nd from 9:00AM to 12:00PM CST.

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Primary view of Combustion of gaseous hydrogen at low pressures in a 35 degree sector of a 28-inch-diameter ramjet combustor
Kerslake, William R.
April 22, 1958
Primary view of Comparison of Several Methods of Cyclic De-Icing of a Gas-Heated Airfoil
Gray, Vernon H. & Bowden, Dean T.
June 22, 1953
Primary view of Effect of Design Variables on Performance of Mach 4.0 Hydrogen Expansion Engines
Dugan, James F., Jr.
July 22, 1958
Primary view of Performance of Five Short Multielement Turbojet Combustors for Hydrogen Fuel in Quarter-Annulus Duct
Jones, Robert E. & Rayle, Warren D.
July 22, 1958
Primary view of Flight Investigation of Pentaborane Fuel in 9.75-inch-diameter Ram-jet Engine With Downstream Fuel Injection
Disher, John H. & Jones, Merle L.
April 22, 1957
Primary view of Performance of a Double-Ramp Side Inlet With Combinations of Fuselage, Ramp, and Throat Boundary-Layer Removal, Mach Number Range, 1.5 to 2.0
Simon, Paul C.
October 22, 1956
Primary view of The Effect of Compressor-Inlet Water Injection on Engine and Afterburner Performance
Sivo, Joseph N.; Wanhainen, John P. & Jones, William L.
July 22, 1958
Primary view of Examination of Recent Lateral-Stability-Derivative Data
Malvestuto, Frank S., Jr. & Kuhn, Richard E.
October 22, 1953
Primary view of Pressure Distributions on the Blade Sections of the NACA 10-(3)(090)-03 Propeller Under Operating Conditions
Johnson, Peter J.
March 22, 1950
Primary view of Investigation of stage performance of X24C-2 ten-stage axial-flow compressor at design speed
Finger, Harold B.; Cohen, Leo & Stewart, Warner L.
May 22, 1950
Primary view of High-speed aerodynamic characteristics of a lateral-control model 3: section characteristics, fence studies, and tabulated pressure coefficients with modified NACA 0012-64 section, 26.6-percent-chord, plain aileron, 0 and 45 degree sweepback
Krumm, Walter J. & Cleary, Joseph W.
November 22, 1950
Primary view of A Preliminary Experimental and Analytical Evaluation of Diborane as a Ram-Jet Fuel
Gammon, Benson E.; Genco, Russell S. & Gerstein, Melvin
December 22, 1950
Primary view of Dynamic Longitudinal Stability and Control of Tandem Coupled Bomber-Fighter Airplane Models With Rigid and Pitch-Free Couplings
Grana, David C. & Hewes, Donald E.
January 22, 1951
Primary view of Investigation of mechanisms of blade failure of forged Hastelloy B and cast Stellite 21 turbine blades in turbojet engine
Yaker, C.; Robards, C. F. & Garrett, F. B.
August 22, 1951
Primary view of Investigation of Low-Speed Lateral Control and Hinge-Moment Characteristics of a 20-Percent-Chord Plain Aileron on a 47.7 Degrees Sweptback Wing of Aspect Ratio 5.1 at a Reynolds Number of 6.0 X 10(Exp 6)
Hadaway, William M. & Salmi, Reino J.
October 22, 1951
Primary view of Influence of airfoil trailing-edge angle and trailing-edge-thickness variation on the effectiveness of a plain flap at high subsonic Mach numbers
Hemenover, Albert D. & Graham, Donald J.
May 22, 1951
Primary view of An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degree Sweepback: Force Characteristics of the Complete Configuration and Its Various Components at Mach Numbers of 1.40 and 1.59
Smith, Norman F. & Marte, Jack E.
January 22, 1951
Primary view of Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds: wing and fuselage pressure distribution
Cleary, Joseph W. & Mellenthin, Jack A.
June 22, 1950
Primary view of The Use of Area Suction for the Purpose of Delaying Separation of Air Flow at the Leading Edge of a 63 Degree Swept-Back Wing
Cook, Woodrow L.; Griffin, Roy N., Jr. & McCormack, Gerald M.
November 22, 1950
Primary view of Interpretation of boundary-layer pressure-rake data in flow with a detached shock
Luidens, Roger W. & Madden, Robert T.
December 22, 1950
Primary view of 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
Cohen, Robert J.
May 22, 1951
Primary view of The torsional deflections of several propellers under operating conditions
Gray, W. H. & Allis, A. E.
June 22, 1951
Primary view of Performance characteristics of aircraft cooling ejectors having short cylindrical shrouds
Kochendorfer, Fred D. & Rousso, Morris D.
May 22, 1951
Primary view of Calculations of Laminar Heat Transfer Around Cylinders of Arbitrary Cross Section and Transpiration-Cooled Walls With Application to Turbine Blade Cooling
Eckert, E. R. G. & Livingood, J. N. B.
June 22, 1951
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