Search Results

Primary view of Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data
Burrows, Dale L.
June 17, 1954
Primary view of Distribution of losses behind a compressor rotor as measured by a rotating rake
Godwin, William R.
January 17, 1956
Primary view of An experimental study of a method for designing fuselage side air inlets for high performance at transonic and low supersonic speeds
Howell, Robert R. & Trescot, Charles D., Jr.
January 17, 1955
Primary view of Effect of large negative dihedral of the horizontal tail on longitudinal and lateral stability characteristics of a swept-wing configuration at transonic speeds
Arabian, Donald D.
January 17, 1956
Primary view of Comparison of Performance and Component Frontal Areas of Hypothetical Two-Spool and One-Spool Turbojet Engines
Dugan, James F., Jr.
January 17, 1956
Primary view of Effects of compressor interstage bleed and adjustable inlet guide vanes on compressor stall characteristics of a high-pressure-ratio turbojet engine at altitude
Mallett, William E. & Groesbeck, Donald E.
January 17, 1956
Primary view of Some interference effects that influence vertical-tail loads at supersonic speeds
Edwards, S. Sherman
February 17, 1956
Primary view of Investigation at Supersonic Speeds of the Effect of Jet Mach Number and Divergence Angle of the Nozzle Upon the Pressure of the Base Annulus of a Body of Revolution
Bromm, August F., Jr. & O'Donnell, Robert M.
December 17, 1954
Primary view of The effect of stick-force gradient and stick gearing on the tracking accuracy of a fighter airplane
Abramovitz, Marvin & Van Dyke, Rudolph D., Jr.
December 17, 1954
Primary view of Analysis of Turbulent Heat Transfer, Mass Transfer, and Friction in Smooth Tubes at High Prandtl and Schmidt Numbers
Deissler, Robert G.
February 17, 1954
Primary view of An Investigation of the Effects of Jet Exhaust and Reynolds Number Upon the Flow Over the Vertical Stabilizer and Rudder of the Douglas D-558-II Research Airplane at Mach Numbers of 1.62, 1.93, and 2.41
Grigsby, Carl E.
June 17, 1954
Primary view of Effect of ground interference on the aerodynamic and flow characteristics of a 42 degree sweptback wing at Reynolds numbers up to 6.8 x 10(6)
Furlong, G. Chester & Bollech, Thomas V.
December 17, 1954
Primary view of Lift Hysteresis at Stall as an Unsteady Boundary-Layer Phenomenon
Moore, Franklin K.
August 17, 1955
Primary view of Thrust and pumping characteristics of a series of ejector-type exhaust nozzles at subsonic and supersonic flight speeds
Hearth, Donald P. & Valerino, Alfred S.
November 17, 1954
Primary view of The dynamic-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements
Triplett, William C.; Brown, Stuart C. & Smith, G. Allan
September 17, 1952
Primary view of A correlation by means of transonic similarity rules of experimentally determined characteristics of a series of symmetrical and cambered wings of rectangular plan form
McDevitt, John B.
December 17, 1951
Primary view of Thrust and Pumping Characteristics of a Series of Ejector-type Exhaust Nozzles at Subsonic and Supersonic Flight Speeds
Hearth, Donald P. & Valerino, Alfred S.
November 17, 1954
Primary view of Compatibility of Metals with Liquid Fluorine at High Pressures and Flow Velocities
Schmidt, Harold W.
April 17, 1958
Primary view of Transonic Aerodynamic and Trim Characteristics of a Multi-Engine Delta-Wing Airplane Model
Swihart, John M. & Foss, Willard E., Jr.
February 17, 1956
Primary view of Some Interference Effects That Influence Vertical-Tail Loads at Supersonic Speeds
Edwards, S. Sherman
February 17, 1956
Primary view of Aerodynamic Performance and Static Stability and Control of Flat-Top Hypersonic Gliders at Mach Numbers From 0.6 to 18
Syvertson, Clarence A.; Gloria, Hermilo R. & Sarabia, Michael F.
September 17, 1958
Primary view of Investigation of the possibility of simplifying missile guidance systems by the use of free-floating flaps and spring-mounted control surfaces
Hikido, Katsumi; Hayashi, Paul H. & Lessing, Henry C.
May 17, 1956
Primary view of Aerodynamic Loads on an External Store Adjacent to an Unswept Wing at Mach Numbers Between 0.75 and 1.96
Hadaway, William M.
February 17, 1956
Primary view of An Experimental Investigation of the Base Pressure Characteristics of Nonlifting Bodies of Revolution at Mach Numbers From 2.73 to 4.98
Reller, John O., Jr. & Hamaker, Frank M.
March 17, 1955
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