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Primary view of Base pressures measured on several parabolic-arc bodies of revolution in free flight at Mach numbers from 0.8 to 1.4 and at large Reynolds numbers
Katz, Ellis & Stoney, William E., Jr.
October 26, 1951
Primary view of Calculated Performance of a Mercury-Compressor-Jet Powered Airplane Using a Nuclear Reactor as an Energy Source
Doyle, R. B.
September 26, 1951
Primary view of Effect of a deflectable wing-tip control on the low-speed lateral and longitudinal characteristics of a large-scale wing with the leading edge swept back 47.5 degrees
Lange, Roy H. & Fink, Marvin P.
April 26, 1951
Primary view of The Effect of Raking the Aileron Tips on the Lateral-Control and Hinge-Moment Characteristics of a 20-Percent-Chord Partial-Span Outboard Aileron on a Wing With Leading-Edge Swept Back 51.3 Degrees
Hammond, Alexander D.
November 26, 1951
Primary view of Effect of Surface Finish on Fatigue Properties at Elevated Temperatures 1: Low-Carbon N-155 With Grain Size of A.S.T.M. 1
Ferguson, Robert R.
June 26, 1951
Primary view of Experimental Investigation of Flow in the Rotating Passages of a 48-Inch Impeller at Low Tip Speeds
Michel, Donald J.; Ginsburg, Ambrose & Mizisin, John
June 26, 1951
Primary view of Free-flight performance of 16-inch diameter supersonic ram-jet units 4: performance of ram-jet units designed for combustion chamber inlet Mach number of 0.21 at free-stream Mach number of 1.6 over a range flight conditions
Rabb, Leonard & North, Warren J.
February 26, 1951
Primary view of Free-Spinning Tunnel Investigation of a 1/20-Scale Model of the Douglas X-3 Airplane
Hultz, Burton E.
December 26, 1951
Primary view of Investigation of wing-tip ailerons on a 51.3 degrees sweptback wing at transonic speeds by the transonic-bump method
Moseley, William C., Jr. & Watson, James M.
November 26, 1951
Primary view of Low-Speed Characteristics of a Wing Having 63 Degrees Sweepback and Uniform Camber
Rose, Leonard M.
June 26, 1951
Primary view of Measurement of distortion in second experimental control rod for argonne naval reactor with constant transverse temperature gradient and uniform longitudinal temperature distribution
Nagey, T. F. & Lietzke, A. F.
September 26, 1951
Primary view of Measurement of distortion in second experimental control rod with temperature patterns simulating shim rod out and shim rod 50 percent inserted for Argonne Naval Reactor
Lietzke, A. F. & Nagey, T. F.
September 26, 1951
Primary view of The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions
Ferri, Antonio & Nucci, Louis M.
January 26, 1951
Primary view of Resistance of Various Materials to Attack by Molten Bismuth-Lead Eutectic at Elevated Temperatures
Gangler, James J. & Engel, Walter J.
September 26, 1951
Primary view of Some Effects of Blade Trailing-Edge Thickness on Performance of a Single-Stage Axial-Flow Compressor
Moses, J. J. & Serovy, G. K.
October 26, 1951
Primary view of Stability and Control Measurements Obtained during USAF-NACA Cooperative Flight-Test Program on the X-4 Airplane (USAF No. 46-677)
Sadoff, Melvin; Ankenbruck, Herman O. & O'Hare, William
October 26, 1951
Primary view of Survey of Available Information on Internal Flow Losses Through Axial Turbomachines
Wu, Chung-Hua
January 26, 1951
Primary view of Wind-Tunnel Investigation at Mach Numbers From 0.50 to 1.29 of an Unswept, Tapered Wing of Aspect Ratio 2.67 With Leading- and Trailing-Edge Flaps - Flaps Deflected in Combination
Stivers, Louis S., Jr. & Malick, Alexander W.
February 26, 1951
Primary view of Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept, tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - leading-edge flaps deflected
Stivers, Louis S., Jr. & Malick, Alexander W.
February 26, 1951
Primary view of Wing-Flow Study of Pressure-Drag Reduction at Transonic Speed by Projecting a Jet of Air From the Nose of a Prolate Spheroid of Fineness Ratio 6
Lopatoff, Mitchell
October 26, 1951
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