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Primary view of Effects of double-slotted flaps and leading-edge modifications on the low-speed characteristics of a large-scale 45 degrees swept-back wing with and without camber and twist
James, Harry A. & Dew, Joseph K.
July 23, 1951
Primary view of Experimental investigation of typical constant- and variable-area exhaust nozzles and effects on axial-flow turbojet-engine performance
Wallner, Lewis E. & Wintler, John T.
July 9, 1951
Primary view of A simplified instrument for recording and indicating frequency and intensity of icing conditions encountered in flight
Perkins, Porter J.; McCullough, Stuart & Lewis, Ralph D.
July 3, 1951
Primary view of The Use of Two-Dimensional Section Data to Estimate the Low-Speed Wing Lift Coefficient at Which Section Stall First Appears on a Swept Wing
Maki, Ralph L.
July 27, 1951
Primary view of A flight study of requirements for satisfactory lateral oscillatory characteristics of fighter aircraft
Liddell, Charles J., Jr.; Creer, Brent Y. & Van Dyke, Rudolph D., Jr.
July 25, 1951
Primary view of Free-Spinning Tunnel Investigation of a 1/20-Scale Model of the McDonnell F2H-3 Airplane
Wilson, Jack H.
July 24, 1951
Primary view of System Analyses and Autopilot Design for Automatic Roll Stabilization of a Supersonic Pilotless Aircraft
Zarovsky, Jacob
July 11, 1951
Primary view of Supplementary Free-Spinning-Tunnel Investigation of a 1/30-Scale Model of the Grumman XF10F-1 Airplane in the Swept-Wing Configuration with Slats Extended
Berman, Theodore & Klinar, Walter J.
July 24, 1951
Primary view of Apparatus for obtaining a supersonic flow of very short duration and some drag measurements obtained with its use
Yeates, John E., Jr.; Bailey, F. J., Jr. & Voglewede, T. J.
July 23, 1951
Primary view of Evaluation of Centrifugal Compressor Performance With Water Injection
Beede, William L.; Hamrick, Joseph T. & Withee, Joseph R., Jr.
July 18, 1951
Primary view of Free-Flight Investigation of the Longitudinal Stability and Control of a Rocket-Propelled Missile Model Having Cruciform, Triangular, Interdigitated Wings and Tails
Sandahl, Carl A. & Hall, James R.
July 10, 1951
Primary view of A Finite Step Method for the Calculation of Span Loadings of Unusual Plan Forms
Campbell, George S.
July 16, 1951
Primary view of Altitude-Test-Chamber Investigation of Performance of a 28-Inch Ram-Jet Engine 4: Effect of Inlet-Air Temperature, Combustion-Chamber-Inlet Mach Number, and Fuel Volatility on Combustion Performance
Kahn, Robert W.; Nakanishi, Shigeo & Harp, James L., Jr.
July 27, 1951
Primary view of An Investigation of Flow Characteristics at Mach Number 4.04 Over 6- and 9-Percent-Thick Symmetrical Circular-Arc Airfoils Having 30-Percent-Chord Trailing-Edge Flaps
Ulmann, Edward F. & Lord, Douglas R.
July 19, 1951
Primary view of Velocity and temperature fields in circular jet expanding from choked nozzle into quiescent air
Rousso, Morris D. & Kochendorfer, Fred D.
July 12, 1951
Primary view of An Experimental Investigation at Subsonic Speeds of a Scoop-Type Air-Induction System for a Supersonic Airplane
Holzhauser, Curt A.
July 19, 1951
Primary view of Theoretical Investigation of an Automatic Control System With Primary Sensitivity to Normal Accelerations as Used to Control a Supersonic Canard Missile Configuration
Seaberg, Ernest C. & Smith, Earl F.
July 10, 1951
Primary view of Compilation and review of effects of design parameters on ditching characteristics
Fisher, Lloyd J. & Hoffman, Edward L.
July 10, 1951
Primary view of Flight Investigation of the Drag of Round-Nosed Bodies of Revolution at Mach Numbers From 0.6 to 1.5 Using Rocket-Propelled Test Vehicles
Hart, Roger G.
July 25, 1951
Primary view of Effects of humidity during fabrication on some physical properties of glass-fabric unsaturated-polyester laminates
Wier, John E.; Pons, Dorothy C. & Axilrod, Benjamin M.
July 18, 1951
Primary view of Power Unit for High-Intensity Light Source
Young, Allen E.; McCullough, Stuart & Smith, Richard L.
July 9, 1951
Primary view of Effects of spanwise thickness variation on the aerodynamic characteristics of 35 degree and 45 degree sweptback wings of aspect ratio 6: transonic-bump method
Morrison, William D., Jr. & Fournier, Paul G.
July 10, 1951
Primary view of Low-Speed Investigation of Several Types of Split Flap on a 47.7 Degree Sweptback-Wing - Fuselage Combination of Aspect Ratio 5.1 at a Reynolds Number of 6.0 X 10(Exp 6)
Spooner, Stanley H. & Mollenberg, Ernst F.
July 10, 1951
Primary view of Characteristics throughout the subsonic speed range of a plane wing and of a cambered and twisted wing, both having 45 degrees of sweepback
Johnson, Ben H., Jr. & Shibata, Harry H.
July 12, 1951
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