37 Matching Results

Search Results

Results: 1 - 24 next
Primary view of Corrosion Tests : SAE 1010 Mild Steel in Synthetic Neutralized Redox Waste Solution
Endow, Noborn
November 13, 1952
Primary view of Investigation of Sulfamic Acid Tank Valve Failures
Endow, N.
November 13, 1952
Primary view of Effects of Free-Stream Reynolds Number, Engine Installation, and Model Scale on Stability Characteristics of a Translating-Spike Inlet at Mach 2.0
Musial, Norman T. & Bowditch, David
November 13, 1957
Primary view of A Wind-Tunnel Investigation of the Stability of the Antisubmarine Rocket Mk 1 Mod 0
Lichtenstein, Jacob H. & Williams, James L.
November 13, 1952
Primary view of Thermal Stability of a Commercial Propyl Pentaborane (HEF-2) in the Range 147 Degree to 190 Degree C
McDonald, G.
November 13, 1957
Primary view of An investigation of the effect of tip shape on the low-speed aerodynamic characteristics of large-scale swept wings
Walling, Walter C.
November 13, 1947
Primary view of Low-Speed Characteristics in Pitch of a 42 Degree Sweptback Wing With Aspect Ratio 3.9 and Circular-Arc Airfoil Sections
Neely, Robert H. & Koven, William
November 13, 1947
Primary view of Investigation of the Dynamic Longitudinal Stability of Two Equal Size Models Coupled in Tandem with a Single Joint: Preliminary Model Flight Tests
Shanks, Robert E. & Grana, David C.
November 13, 1950
Primary view of Effect of Magnitude of Vibratory Load Superimposed on Mean Tensile Load on Mechanism of and Time to Fracture of Specimens and Correlation to Engine Blade
Ferguson, Robert R.
November 13, 1952
Primary view of Effect of radiant energy on vaporization and combustion of liquid fuels
Berlad, A. L. & Hibbard, R. R.
November 13, 1952
Primary view of Performance characteristics of several types of axially symmetric nose inlets at Mach number 3.85
Connors, James F. & Woollett, Richard R.
November 13, 1952
Primary view of Some observations of flow at the throat of a two-dimensional diffuser at a Mach number of 3.85
Connors, James F. & Woollett, Richard R.
November 13, 1952
Primary view of Factors in selecting fuels for gas-turbine powered aircraft
Gibbons, Louis C.
November 13, 1950
Primary view of Ability of Pilots to Control Simulated Short-Period Yawing Oscillations
Phillips, William H. & Cheatham, Donald C.
November 13, 1950
Primary view of Wire cloth as porous material for transpiration-cooled walls
Eckert, E. R. G.; Kinsler, Martin R. & Cochran, Reeves P.
November 13, 1951
Primary view of Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) 1: body of revolution with near-parabolic forebody and cylindrical afterbody
Jack, John R. & Burgess, Warren C.
November 13, 1951
Primary view of Effect of afterbody length and keel angle on minimum depth of step for landing stability and on take-off stability of a flying boat
Olson, Roland E. & Land, Norman S.
November 13, 1947
Primary view of Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data
Sivells, James C. & Westrick, Gertrude C.
November 13, 1950
Primary view of Effect of chord size on weight and cooling characteristics of air-cooled turbine blades
Esgar, Jack B.; Schum, Eugene F. & Curren, Arthur N.
November 13, 1956
Primary view of Steady Steady State Temperature Distribution in a Thin Cylindrical Shell With Piecewise Variation of External Heat Transfer Coefficient, External Coolant Temperature, and Internal Heat Input
Abernathy, Fred H.
November 13, 1959
Primary view of The Determination of Hydrogen in Magnesium, Lithium, and Magnesium Alloys
Mallett, Manley William, 1909-; Gerds, A. F. & Griffith, C. B.
November 13, 1951
Primary view of General Reactor-Engineering Research Quarterly Progress Report [for] Period Ending August 31, 1950
Lyon, R. N.
November 13, 1950
Primary view of Army Gas-Cooled Reactor Systems Program Quarterly Progress Report: July 1 - September 30, 1964
Aerojet-General Corporation
November 13, 1964
Primary view of Thermal Stability of a Commercial Propyl Pentaborane (HEF-2) in the Range 147 to 190 Degrees C
McDonald, G.
November 13, 1957
Back to Top of Screen