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Synonyme wurden verwendet für: AIRFOILS • DISTRIBUTION • PRESSURE • PRESSURE DISTRIBUTION
Suche ohne Synonyme: keywords:(PRESSURE DISTRIBUTION - AIRFOILS - NACA 0012)

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

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

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

    Aerodynamic Characteristics of a Number of Modified NACA Four-digit-series Airfoil Sections

    Loftin, Laurence K , Jr / Cohen, Kenneth S | NTRS | 1948
    Schlagwörter: AIRFOILS - NACA 0010-64 - ORDINATES , AIRFOILS - NACA 0010-65 - ORDINATES , AIRFOILS - NACA 0010-34 - CHAR , A C , MOMENTS & ORDINATES , AIRFOILS - NACA 0010-35 - CHAR , A C , MOMENTS & ORDINATES , AIRFOILS - NACA 0010-66 - ORDINATES , AIRFOILS - NACA 0012-64 - CHAR , A C , MOMENTS & ORDINATES , WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE WORK CARRIED ON AT LMAL , AIRFOILS - NACA 0008-34 - ORDINATES , AIRFOILS - NACA 0012-34 - ORDINATES

    Investigation of NACA 64,2-432 and 64,3-440 Airfoil Sections with Boundary-layer Control and an Analytical Study of Their Possible Applications

    Horton, Elmer A / Racisz, Stanley Frank / Paradiso, Nicholas J | NTRS | 1951
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - NACA 64,3-040 , AIRFOILS - NACA 64,3-440 (A=1 0)(MOD ) - CHAR & ORDINATES , BOUNDARY LAYER CONTROL - AIRFOILS - NACA 64,3-440 (A=1 0)(MOD ) , AIRFOILS - NACA 64,3-040 - ORDINATES , AIRFOILS - NACA 64,2-432 - CHAR & ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 64,2-032 , AIRFOILS - NACA 64,2-032 - ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 64,2-432 , BOUNDARY LAYER CONTROL - AIRFOILS - NACA 64,2-432 , PRESSURE DISTRIBUTION - AIRFOILS - NACA 64,3-440 (A=1 0)(MOD )

    Comparisons of theoretical and experimental lift and pressure distributions on airfoils in cascade

    Katzoff, S / Bogdonoff, Harriet E / Boyet, Howard | NTRS | 1947
    Schlagwörter: AIRFOILS - NACA 65-410 - CHARACTERISTICS LOW-DRAG (BLOWER BLADE) , AIRFOILS - CASCADES , AIRFOILS - NACA 65-810 - CHARACTERISTICS LOW-DRAG (BLOWER BLADE) , PRESSURE DISTRIBUTION - AIRFOILS - NACA 65-(12)10 , PRESSURE DISTRIBUTION - AIRFOILS - CASCADES , AIRFOILS - NACA 65-(12)10 - CHARACTERISTICS LOW-DRAG (BLOWER BLADE) , PRESSURE DISTRIBUTION - AIRFOILS - NACA 65-810

    Effects of compressibility on maximum lift coefficients for six propeller airfoils

    Cleary, Harold E | NTRS | 1945
    Schlagwörter: AIRFOILS, CAMBERED - CHARACTERISTICS , AIRFOILS - NACA 16-715 - CHARACTERISTICS PROPELLER , AIRFOILS - NACA 16-515 - CHARACTERISTICS PROPELLER , PRESSURE DISTRIBUTION - AIRFOILS - NACA 16-215 , AIRFOILS - NACA 16-509 - CHARACTERISTICS PROPELLER , AIRFOILS - NACA16-709 - CHARACTERISTICS PROPELLER , PRESSURE DISTRIBUTION - AIRFOILS - NACA 16-515 , PRESSURE DISTRITUTION - AIRFOILS - NACA 16-715 , AIRFOILS - NACA 16-209 - CHARACTERISTICS PROPELLER , WIND TUNNEL TESTS (NACA-HIGH-SPEED-8')

    Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel

    Stivers, Louis S , Jr | NTRS | 1944
    Schlagwörter: AIRFOILS-NACA 652-415-CHAR , MOMENTS & ORDINATES LOW-DRAG , PRESSURE DISTRIBUTION-AIRFOILS NACA 64,2-015(MOD ) , AIRFOILS-NACA 64,2-015(MOD )-ORDINATES LOW-DRAG , PRESSURE DISTRIBUTION-AIRFOILS NACA 747A315 , AIRFOILS-NACA 747A315-CHAR , MOMENTS & ORDINATES LOW-DRAG , AIRFOILS-NACA-7-SERIES , AIRFOILS-NACA 747A415-CHAR , MOMENTS & ORDINATES LOW-DRAG , PRESSURE DISTRIBUTION-AIRFOILS NACA 747A415 , AIRFOILS-NACA-CLASSIFICATION LOW-DRAG , WIND TUNNEL TESTS-NACA-PRESSURE, TWO-DIMENSIONAL LMAL (7 1/2' X 3')

    Low-speed characteristics of four cambered, 10-percent-thick NACA airfoil sections

    Mccullough, George B / Haire, William M | NTRS | 1950
    Schlagwörter: AIRFOILS, CAMBERED , AIRFOILS - NACA 0010 (A=0 8, CLI=0 8) - CHAR , MOMENTS & ORDINATES , AIRFOILS - CHARACTERISTICS , AIRFOILS - NACA 0010 (A=1 0, CLI=0 3) - CHAR , MOMENTS & ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 64A810 (A=0 8) , PRESSURE DISTRIBUTION - AIRFOILS-NACA 0010 (A=1 0, CLI=0 3) , AIRFOILS - NACA 64A310 - CHAR , MOMENTS & ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS-NACA 64A310 , AIRFOILS - NACA 64A810 (A=0 8) - CHAR , MOMENTS & ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS-NACA 0010 (A=0 8, CLI=0 8)

    Low-speed Tests of Five NACA 66-series Airfoils Having Mean Lines Designed to Give High Critical Mach Numbers

    Von Doenhoff, Albert E / Stivers, Louis S / O'Connor, James M | NTRS | 1947
    Schlagwörter: AIRFOILS - NACA 66(215)-016 LOW-DRAG , PRESSURE DISTRIBUTION - AIRFOILS - NACA 66(215)-316 , PRESSURE DISTRIBUTION - AIRFOILS - NACA 66(215)-416 , AIRFOILS - NACA 66(215)-416 - CHAR , A C , MOMENTS & ORDINATES , AIRFOILS - NACA 66(215)-316 - CHAR , A C , MOMENTS & ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 66(215)-216 , AIRFOILS - NACA 66(215)-216 - CHAR , A C , MOMENTS & ORDINATES

    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 , THEORIES - AIRFOILS, THIN , CHARTS - AIRFOILS , AIRFOILS - ANGLE OF ZERO LIFT , AIRFOILS - THICKNESS , PRESSURE DISTRIBUTION - AIRFOILS - NACA 654-421

    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") , WIND TUNNEL WALL INTERFERENCE - AIRFOILS , PHOTOGRAPHY - AIR FLOW - AIRFOILS - SCHLIEREN METHOD , AIR FLOW - AIRFOILS - 2-DIMENSIONAL , AIRFOILS - NACA 66,2-015 - LOW-DRAG

    Effect of Compressibility on the Distribution of Pressures over a Tapered Wing of NACA 230-series Airfoil Sections

    Pearson, E O , Jr | NTRS | 1947
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - NACA 233016-23009 , WIND TUNNEL TESTS - NACA - HIGH-SPEED (16') , AIRFOILS - ANGLE OF ATTACK , PRESSURE DISTRIBUTION - AIRFOILS - NACA 230-SERIES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 23016-23009 , PRESSURE DISTRIBUTION - WINGS, TAPERED-EFFECT OF COMPRESSIBILITY

    Effects of Propellers and of Vibration on the Extent of Laminar Flow on the NACA 27-212 Airfoil

    Gaydos, M Edward | NTRS | 1939
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - NACA 27-212 , AIRFOILS - NACA - LAMINAR-FLOW , AIRFOILS - NACA 27-212 LAMINAR-FLOW , WIND TUNNEL TESTS - NACA - HIGH-SPEED (8') , BOUNDARY LAYER - AIRFOILS LAMINAR

    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 , AIRFOILS - ASPECT RATIO, SMALL , CENTER OF PRESSURE - WINGS, DELTA , PRESSURE DISTRIBUTION - WINGS, DELTA

    A Study of Flow Changes Associated with Airfoil Section Drag Rise at Supercritical Speeds

    Nitzberg, Gerald E / Crandall, Stewart | NTRS | 1949
    Schlagwörter: AIRFOILS - NACA 641-210 - CHARACTERISTICS LOW-DRAG , AIRFOILS - NACA 23015 - CHARACTERISTICS , AIRFOILS - NACA 66,2-215 (A-0 6) LOW-DRAG , AIRFOILS - NACA 652-215 (A-0 5) LOW-DRAG , AIRFOILS - NACA 4415 , PRESSURE DISTRIBUTION - AIRFOILS - NACA 23015 - EFFECT OF COMPRESSIBILITY , AIRFOILS - NACA 641-208 - CHARACTERISTICS LOW-DRAG , AIRFOILS - NACA 641-206 - CHARACTERISTICS LOW-DRAG , AIRFOILS - NACA 0015

    Some Effects of Reynolds and Mach Numbers on the Lift of an NACA 0012 Rectangular Wing in the NACA 19-Foot Pressure Tunnel

    Muse, Thomas C | NTRS | 1943
    Schlagwörter: WIND TUNNEL TESTS - NACA - PRESSURE (19') , LIFT COEFFICIENTS - AIRFOILS - NACA 0012

    Variation of Peak Pitching-Moment Coefficients for Six Airfoils as Affected by Compressibility

    Cleary, Harold E | NTRS | 1944
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - NACA 16-SERIES , AIRFOILS - NACA 16-715 - MOMENTS - PROPELLER , AIRFOILS - NACA 16-215 - MOMENTS - PROPELLER , AIRFOILS - NACA 16-209 - MOMENTS - PROPELLER , PITCHING MOMENTS - AIRFOILS - NACA 16-SERIES , AIRFOILS - NACA 16-515 - MOMENTS - PROPELLER , AIRFOILS - NACA 16-709 - MOMENTS - PROPELLER , AIRFOILS - NACA 16-509 - CHAR & MOMENTS - PROPELLER , WIND TUNNEL TESTS (NACA-HIGH-SPEED-8')

    An Application of Lifting-surface Theory to the Prediction of Angle-of-attack Hinge-moment Parameters for Aspect Ratio 4.5 Wings

    Jones, Arthur L / Flanagan, Mildred G / Sluder, Loma | NTRS | 1947
    Schlagwörter: AIRFOILS - NACA 0012-64 (MOD ) - TAIL SURFACE , LOAD DISTRIBUTION, WING-SPAN , LIFT DISTRIBUTION - WINGS , AIRFOILS - NACA 0009-0015 - LOW-DRAG (TAIL SURFACE) , AIRFOILS - NACA 65(216)-014 - LOW-DRAG (TAIL SURFACE) , AIRFOILS - ANGLE OF ATTACK , AIRFOILS - ASPECT RATIO , THEORIES - AIRFOILS - LIFTING-SURFACE

    Aerodynamic Characteristics of the NACA 8-H-12 Airfoil Section at Six Reynolds Numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6).

    Schaefer, Raymond F / Smith, Hamilton A | NTRS | 1949
    Schlagwörter: AIRFOILS - NACA 8-H-12 - CHAR , A C , MOMENTS & ORDINATES LOW-DRAG , AIRFOILS - CHARACTERISTICS EFFECT OF SURFACE ROUGHNESS , AIRFOILS - NACA 0012 - CHARACTERISTICS , AIRFOILS - NACA 23012 - CHARACTERISTICS , WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE ( 7 1/2'X 3')

    Further comparisons of theoretical and experimental lift and pressure distributions on airfoils in cascade at low-subsonic speed

    Katzoff, Samuel / Hannah, Margery E | NTRS | 1951
    Schlagwörter: AIRFOILS - NACA 65-(12A)10 , BOUNDARY LAYER - AIRFOILS - CASCADES , FLOW - AIRFOILS - CASCADES , FLOW VELOCITY - DISTRIBUTION , THEORIES - AIRFOILS , PRESSURE DISTRIBUTION - AIRFOILS - CASCADES , AIRFOILS - NACA 65-(12)10

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