National Advisory Committee for Aeronautics (NACA) - 13,786 Matching Results

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Primary view of Experimental Investigation of a New Type of Low-Drag Wing-Nacelle Combination
Allen, H. Julian & Frick, Charles W., Jr.
July 1942
Primary view of A method for calculating heat transfer in the laminar flow region of bodies
Allen, H. Julian & Look, Bonne C.
December 1942
Primary view of A method for calculating heat transfer in the laminar flow region of bodies
Allen, H. Julian & Look, Bonne C.
1943
Primary view of Problems of performance and heating of hypersonic vehicles
Allen, H. Julian & Neice, Stanford E.
March 5, 1956
Primary view of The Effect of Compressibility on the Growth of the Laminar Boundary Layer on Low-Drag Wings and Bodies
Allen, H. Julian & Nitzberg, Gerald E.
July 1947
Primary view of The Effect of Compressibility on the Growth of the Laminar Boundary Layer on Low-Drag Wings and Bodies
Allen, H. Julian & Nitzberg, Gerald E.
January 1943
Primary view of Characteristics of flow over inclined bodies of revolution
Allen, H. Julian & Perkins, Edward W.
March 5, 1951
Primary view of A study of effects of viscosity on flow over slender inclined bodies of revolution
Allen, H. Julian & Perkins, Edward W.
1951
Primary view of Wall interference in a two-dimensional-flow wind tunnel with consideration of the effect of compressibility
Allen, H. Julian & Vincenti, Walter G.
December 1944
Primary view of Wall interference in a two-dimensional-flow wind tunnel, with consideration of the effect of compressibility
Allen, H. Julian & Vincenti, Walter G.
1944
Primary view of An Experimental Investigation of Several Low-Drag Wing-Nacelle Combinations with Internal Air Flow
Allen, H. Julian; Frick, Charles W. & Erickson, Myles D.
March 1945
Primary view of The interaction of boundary layer and compression shock and its effect upon airfoil pressure distributions
Allen, H. Julian; Heaslet, Max A. & Nitzberg, Gerald E.
April 10, 1947
Primary view of Heat of Combustion of the Product Formed by the Reaction of Acetylene and Diborane (LFPL-CZ-3)
Allen, Harrison, Jr. & Tannenbaum, Stanley
October 24, 1957
Primary view of A method for the analysis of compounds containing boron, carbon, and hydrogen
Allen, Harrison, Jr. & Tannenbaum, Stanley
March 3, 1955
Primary view of Chemical and Physical Properties of Modified Hi-Cal-2
Allen, Harrison, Jr.; McDonald, Glen E. & Pusanski, Barbara J.
December 1955
Primary view of Visualization study of secondary flows in turbine rotor tip regions
Allen, Hubert W. & Kofskey, Milton G.
September 1955
Primary view of Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with a bypass discharging from the top or bottom of the diffuser in an axial direction
Allen, J. L. & Beke, Andrew
March 23, 1953
Primary view of Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with bypasses discharging in an axial direction
Allen, J. L. & Beke, Andrew
January 30, 1953
Primary view of Performance comparison at supersonic speeds of inlets spilling excess flow by means of bow shock, conical shock, or bypass
Allen, J. L. & Beke, Andrew
October 23, 1953
Primary view of Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane 2: Inlets Utilizing Half of a Conical Spike
Allen, J. L. & Simon, P. C.
September 4, 1952
Primary view of Performance of a blunt-lip side inlet with ramp bleed, bypass, and a long constant-area duct ahead of the engine : Mach number 0.66 and 1.5 to 2.1
Allen, John L.
December 28, 1956
Primary view of Performance of a Blunt-lip Side Inlet With Ramp Bleed, Bypass, and a Long Constant-area Duct Ahead of the Engine- Mach Numbers 0.66 and 1.5 to 2.1
Allen, John L.
December 28, 1956
Primary view of Performance of an Inlet Having a Variable-angle Two-dimensional Compression Surface and a Fixed-geometry Subsonic Diffuser for Application to Reduced Engine Rotative Speeds- Mach Numbers 0.66, 1.5, 1.7, and 2.0
Allen, John L.
January 30, 1958
Primary view of Preliminary investigation of effect on performance of dividing conical-spike nose inlets into halves at Mach numbers 1.5 to 2.0
Allen, John L.
December 19, 1955
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