Synonyme wurden verwendet für: High pressure pressure
Suche ohne Synonyme: keywords:(High pressure)

1–20 von 99 Ergebnissen
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    Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel

    Becker, John V | NTRS | 1940
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - NACA 0012 , PRESSURE DISTRIBUTION - AIRFOILS - NACA 23012 , WIND TUNNEL TESTS - NACA - HIGH-SPEED (8')

    Investigation of Drag and Pressure Distribution of Windshields at High Speeds

    Wright, Ray M | NTRS | 1942
    Schlagwörter: PRESSURE DISTRIBUTION - WINDSHIELDS , WIND TUNNEL TESTS - NACA - HIGH-SPEED (8') , PRESSURE DISTRIBUTION - COCKPIT TOPS , PRESSURE DISTRIBUTION - WINGS - DOUGLAS DC-3 , PRESSURE DISTRIBUTION - FUSELAGES - DOUGLAS DC-3 , WIND TUNNEL TESTS (NACA-HIGH-SPEED-8')

    High-Speed Wind-Tunnel Tests of a 1/6-scale Model of a Twin-Engine Pursuit Airplane

    V. M. Ganzer | NTIS | 1942
    Schlagwörter: Pressure distribution , High velocity , High speed diving

    The effect of altitude on cooling

    Wood, George P | NTRS | 1943
    Schlagwörter: COOLANTS, HIGH-TEMPERATURE-ETHYLENE GLYCOL , FLYING, HIGH-SPEED , ENGINES-PRESSURE DROP

    Wind-Tunnel Investigation of a Low-Drag Airfoil Section with a Double Slotted Flap

    Bogdonoff, Seymour M. | NTRS | 1943
    Schlagwörter: WINGS-HIGH-LIFT DEVICES , WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2' X 3')

    High-altitude Cooling IV : Intercoolers

    Rubert, K F | NTRS | 1944
    Schlagwörter: FLYING, HIGH-ALTITUDE , ENGINES - INTERCOOLERS - PRESSURE DROP

    High-altitude cooling V : cowling and ducting

    Katzoff, S | NTRS | 1944
    Schlagwörter: FLYING, HIGH-ALTITUDE , DUCTS-PRESSURE DROP

    High-altitude cooling I : resume of the cooling problem

    Silverstein, Abe | NTRS | 1944
    Schlagwörter: FLYING, HIGH-ALTITUDE , ENGINES-PRESSURE DROP

    High-altitude Cooling III : Radiators

    Nielsen, Jack N | NTRS | 1944
    Schlagwörter: RADIATORS, DUCT-PRESSURE DROP , FLYING, HIGH-ALTITUDE

    The effects of roughness at high Reynolds numbers on the lift and drag characteristics of three thick airfoils

    Turner, Harold R , Jr | NTRS | 1944
    Schlagwörter: REYNOLDS NUMBER, HIGH , WIND TUNNEL TESTS - NACA - PRESSURE, TWO-DIMENSIONAL

    Flight Investigation of Boundary-Layer Control by Suction Slots on an NACA 35-215 Low-Drag Airfoil at High Reynolds Numbers

    Von Doenhoff, Albert E | NTRS | 1944
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - WING SLOTS NACA 35-215 , REYNOLDS NUMBER, HIGH

    Wind-tunnel Investigation of a High-critical-speed Fuselage Scoop Including the Effects of Boundary Layer

    Baals, Donald D | NTRS | 1945
    Schlagwörter: WIND TUNNEL TESTS - NACA - HIGH-SPEED (8') , PRESSURE DISTRIBUTION - FUSELAGES

    Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube

    Humphreys, Milton D | NTRS | 1945
    Schlagwörter: PRESSURE-EFFECT OF COMPRESSIBILITY & ANGLE OF YAW , WIND TUNNEL TESTS-NACA-HIGH-SPEED (18 INCHES X 4 INCHES)

    Flow of High Pressure Air in Small Pipes

    D. Rendel / J. Rudman | NTIS | 1946
    Schlagwörter: High pressure

    Internal and external aerodynamics of ducted bodies at supersonic speeds

    Brown, Clinton E | NTRS | 1946
    Schlagwörter: AIR FLOW VELOCITY, HIGH - SUPERSONIC , PRESSURE DISTRIBUTION-BODIES

    Pressure distribution over a plug-type spoiler-slot aileron on a tapered wing with full span slotted flaps

    Lowry, John G / Turner, Thomas R | NTRS | 1946
    Schlagwörter: PRESSURE DISTRIBUTION-AILERONS, SPOILER-SLOT (PLUG) , FLYING, HIGH-SPEED

    The stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds

    Ribner, Herbert S | NTRS | 1947
    Schlagwörter: AIR FLOW VELOCITY, HIGH - SUBSONIC , AIR FLOW VELOCITY, HIGH - SUPERSONIC , PRESSURE DISTRIBUTION - WINGS, DELTA

    Theoretical lift distribution and upwash velocities for thin wings at supersonic speeds

    Evvard, John C / Turner, L Richard | NTRS | 1947
    Schlagwörter: AIR FLOW VELOCITY, HIGH - SUPERSONIC , PRESSURE DISTRIBUTION - WINGS, DELTA

    Two-dimensional Wind-tunnel Investigation of the NACA 64(sub 1)-012 Airfoil Equipped with Two Types of Leading-edge Flap

    Fullmer, Felicien F | NTRS | 1947
    Schlagwörter: WINGS - HIGH LIFT DEVICES , WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2 X 3')