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Synonyme wurden verwendet für: distribution • pressure • pressure distribution
Suche ohne Synonyme: keywords:(pressure distribution - airfoil - naca 0012)

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    Prediction of Airfoil Trailing-Edge Noise Using Empirical Wall-Pressure Spectrum Models

    Lee, Seongkyu / Shum, Jessica G. | AIAA | 2019
    Schlagwörter: NACA 0012 , Airfoil Flow , Sound Pressure Level

    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 , AIRFOILS - NACA 0012 - CHARACTERISTICS , AIRFOILS - NACA 23012 - CHARACTERISTICS , PRESSURE DISTRIBUTION - AIRFOILS - NACA 23012 , WIND TUNNEL TESTS - NACA - HIGH-SPEED (8')

    Using Reynolds-Averaged Navier-Stokes Calculations to Predict Trailing-Edge Noise

    Glegg, Stewart / Morin, Bruce / Atassi, Oliver et al. | AIAA | 2010
    Schlagwörter: NACA 0012 , Sound Pressure Level , Airfoil Chord

    Flow of a compressible fluid past a symmetrical airfoil in a wind tunnel and in free air

    Emmons, Howard W | NTRS | 1948
    Schlagwörter: AIRFOILS - NACA 0012 - ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 0012

    Effects of mean-line loading on the aerodynamic characteristics of some low-drag airfoils

    Turner, Harold R , Jr | NTRS | 1943
    Schlagwörter: AIRFOILS, CAMBERED - CHARACTERISTICS WIND TUNNEL TESTS (NACA - PRESSURE - 2-DIME , PRESSURE DISTRIBUTION - AIRFOILS - NACA 653-418 , AIRFOIL SURFACES - ROUGHNESS , PRESSURE DISTRIBUTION - AIRFOILS - NACA 654-421

    Chordwise and spanwise loadings measured at low speed on a triangular wing having an aspect ratio of two and an NACA 0012 airfoil section

    Wick, Bradford H | NTRS | 1948
    Schlagwörter: LOAD DISTRIBUTION, WING-SPAN , AIRFOILS - NACA 0012 - CHARACTERISTICS , CENTER OF PRESSURE - WINGS, DELTA , PRESSURE DISTRIBUTION - WINGS, DELTA

    Tests in the NACA two-dimensional low-turbulence tunnel of airfoil sections designed to have small pitching moments and high lift-drag ratios

    Tetervin, Neal | NTRS | 1943
    Schlagwörter: AIRFOILS-NACA 23015-CHAR , A C , MOMENTS & ORDINATES , PITCHING MOMENTS-AIRFOILS-NACA , AIRFOIL SURFACES-ROUGHNESS , PRESSURE DISTRIBUTION-AIRFOILS-NACA HELICOPTER

    Subsonic two-dimensional-flow conditions near an airfoil determined by static pressures measured at the tunnel wall

    Daley, Bernard N / Hanna, Lillian E | NTRS | 1949
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - NACA 0012 , AIRFOILS - NACA 66,2-215 - LOW-DRAG , WIND TUNNEL TESTS - NACA - HIGH-SPEED (18"X4") , AIRFOILS - NACA 66,2-015 - LOW-DRAG

    Two-dimensional Wind-tunnel Investigation of Sealed 0.22-airfoil-chord Internally Balanced Ailerons of Different Contour on an NACA 65(112)- 213 Airfoil

    Braslow, Albert L | NTRS | 1946
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - NACA 65(112)-213 , AIRFOIL SURFACES - ROUGHNESS , AIRFOILS - NACA 65(112)-213 - CHAR & ORDINATES , WIND TUNNEL TESTS - NACA - PRESSURE,TWO-DIMENSIONAL (LMAL)

    Wind-Tunnel Tests of Ailerons at Various Speeds II : Ailerons of 0.20 Airfoil Chord and True Contour with 0.60 Aileron-Chord Sealed Internal Balance on the NACA 66,2-216 Airfoil

    Bird, J D | NTRS | 1943
    Schlagwörter: AIRFOILS-NACA 66,2-216-CHAR , MOMENTS & ORDINATES LOW-DRAG , PRESSURE DISTRIBUTION-AIRFOIL-NACA 66,2-216 , WIND TUNNEL TESTS-NACA-STABILITY

    Report on the special field "Interference" to the wind-tunnel committee in February 1945

    Schlichting, Hermann / Moller, Egon | NTRS | 1953
    Schlagwörter: PRESSURE DISTRIBUTION - FUSELAGE-WING COMBINATIONS , AIRFOILS - NACA 0012-0 825-40 , AIRFOILS - NACA 0010-0 825-40 , AIRFOILS - NACA 23012 , AIRFOILS - NACA 0015

    Effects of Mach Number up to 0.34 and Reynolds Number up to 8 X 10(exp 6) Power on the Maximum Lift Coefficient of a Wing of NACA 66-series Airfoil Sections

    Furlong, G Chester / Fitzpatrick, James E | NTRS | 1950
    Schlagwörter: PRESSURE DISTRIBUTION - WINGS , AIRFOIL SURFACES - ROUGHNESS , WIND TUNNEL TESTS - NACA - PRESSURE (19 FEET) , AIRFOILS - NACA 66(215)-116(A=0 6) - 66(215)-216(A=0 6)

    Experimental Investigation of the Perpendicular Vortex-Airfoil Interaction of Transonic Speeds

    D. R. Wilson / I. M. Kalkhoran / D. D. Seath | NTIS | 1987
    Schlagwörter: Pressure distribution , NACA-0012 airfoils

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