A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel /

A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel /

Bibliographic Details
Main Author:	Morgan, Harry L.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Other Authors:	Ferris, James C., McGhee, Robert J.
Format:	Government Document Book
Language:	English
Published:	[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.
Series:	NASA technical memorandum ; 89125.
Subjects:	Aerofoils. Reynolds number.

Similar Items

Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
by: Jenkins, Renaldo V.
Published: (1983)

Analysis of experimental data for cast 10-2/DOA 2 supercritical airfoil at low Reynolds numbers and application to high Reynolds number flow = Analyse des données expérimentales de l'aile supercritique cast 10-2/DOA 2 aux faibles nombres de Reynolds et application des résultats aux simulations d'écoulement à des nombres de Reynolds élevés /
by: Chan, Y. Y.
Published: (1989)

High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
by: Mineck, Raymond E.
Published: (1987)

High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
Published: (1982)

Analysis of experimental data for cast 10-2/DOA2 supercritical airfoil at high Reynolds numbers = Analyse de données expérimentales pour le plan supercritique cast 10-2/DOA2 en fonction de nombres de Reynolds élevés /
by: Chan, Y. Y.
Published: (1988)

Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section /
by: Ladson, Charles L.
Published: (1988)

Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter Transonic Cryogenic Tunnel /
by: Jenkins, Renaldo V.
Published: (1988)

A catalog of low Reynolds number airfoil data for wind turbine applications /
by: Miley, Stan J.
Published: (1982)

High Reynolds number tests of the cast 10-2/DOA 2 airfoil in the Langley 0.3-meter transonic cryogenic tunnel - phase II /
Published: (1984)

Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel /
by: McGhee, Robert J.
Published: (1988)

Addendum to a catalog of low Reynolds number airfoil data for wind turbine applications : a subcontract report /
by: Miley, Stan J.
Published: (1985)

Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /
by: Noonan, Kevin W.
Published: (1980)

Flight Mechanics/Estimation Theory Symposium, 1989 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 23-24, 1989 /
Published: (1989)

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /
by: Johnson, William G. (William Garland), 1944-
Published: (1985)

Tests of a NACA 65₁-213 airfoil in the NASA Langley 0.3 meter transonic cryogenic tunnel /
by: Plentovich, Elizabeth B.
Published: (1984)

Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition /
Published: (1987)

Low Reynolds number vehicles /
by: Mueller, T. J.
Published: (1985)

Elliptic flow computation by low Reynolds number two-equation turbulence models /
by: Michelassi, V.
Published: (1991)

Mixing of submerged turbulent jets at low Reynolds numbers /
by: Ungate, Christopher D.
Published: (1975)

Analysis of fluctuating static pressure measurements in a large high Reynolds number transonic cryogenic wind tunnel /
by: Igoe, William B.
Published: (1993)

High Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
by: Ladson, Charles L.
Published: (1987)

Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows /
by: Kim, Sang-Wook
Published: (1988)

On the drag of model dendrite fragments at low Reynolds number /
by: Zakhem, R.
Published: (1993)

Low Reynolds number flow heat exchangers : advanced study institute book /
Published: (1983)

Turbulent boundary-layer studies at high Reynolds numbers at Mach numbers between 0.2 and 2.8 /
by: Winter, K. G.
Published: (1973)

Reynolds-number similarity of orthogonal decomposition of the outer layer of turbulent wall flow /
by: Liu, Zi-Chao
Published: (1994)

A finite element computational method for high Reynolds number laminar flows /
by: Kim, Sang-Wook
Published: (1987)

Heat transfer in low Reynolds number flow /
Published: (1971)

Stagnation region gas injection in low Reynold's number hypersonic flow /
by: Chen, Y. S.
Published: (1967)

Reynolds number influences in aeronautics /
Published: (1993)

Application of shock tubes to transonic airfoil testing at high Reynolds number /
Published: (1978)

Effects of global density and Reynolds number variations on mixing in turbulent, axisymmetric jets /
by: Pitts, William M.
Published: (1986)

Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil /
by: Ferris, James C., et al.
Published: (1987)

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel /
by: Lawing, Pierce L., et al.
Published: (1980)

IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow : proceedings of the IUTAM symposium held in Princeton, NJ, U.S.A., 11-13 September 2002 /
Published: (2004)

Reynolds number effects in transonic flow /
by: Elsenaar, A.
Published: (1988)

Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing /
by: Reubush, David E.
Published: (1976)

Magnetic hypersonic flow near the stagnation point at low Reynolds number /
by: Chen, S. Y.
Published: (1968)

Magnetic hypersonic flow near the stagnation point at low Reynolds number /
by: Chen, S. Y.
Published: (1969)

Measurement of transition on a sphere at high reynolds numbers /
by: Hsu, En Yun
Published: (1957)