Adaptive wall technology for minimization of wall interferences in transonic wind tunnels /

Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic tunnel /

Mineck, Raymond E.
Hill, Acquilla S.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 8-9.Mode of access: Internet

A method for the design of porous-wall wind tunnels /

Stokes, George M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"January 20, 1956."Includes bibliographical references (p. 36).Mode of access: Internet

Turbulent wall jet in a coflowing stream /

Campbell, James F. (James Franklin), 1941-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-19).Mode ...

Reduction of wind-tunnel wall interference by controlled wall flow /

Bernstein, Samuel.
Joppa, Robert G. (Robert Glenn)
University of Washington. Dept. of Aeronautics and Astronautics.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 47-49).Mode of access: Internet

Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques /

Mineck, Raymond E.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 11).Mode of access: Inte...

Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels /

Green, Lawrence L. (Lawrence Lee)
Newman, Perry A.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 18.Mode of access: Internet

Aerofoil testing in a self-streamlining flexible walled wind tunnel /

Lewis, Mark Charles.
Langley Research Center.

January 1988

"May 1988"--Cover."Prepared for Langley Research Center under Grant NSG-7172."Includes bibliographic...

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section /

Mineck, Raymond E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1987

"December 1987"--Cover.Includes bibliographical references (p. 6).Mode of access: Internet

Wind tunnel interference factors for high-lift wings in closed wind tunnels /

Joppa, Robert G. (Robert Glenn)
Langley Research Center.
University of Washington.

"February 1973.""Prepared by University of Washington ... for Langley Research Center."Cover title.I...

Low-speed upwash interference on a transport model in a rectangular slotted-wall wind tunnel /

Mann, Michael J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Support interference of wind tunnel models : a selective annotated bibliography /

Tuttle, Marie H.
Gloss, Blair B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject category 09."March 1981"--Cover."Langley Research Center."Includes bibliographical reference...

Adaptive wall wind tunnels and wall interference correction methods

Hornung, H.
Stanewsky, E. (eds.)
Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt e.V., Goettingen (Germany, F.R.). Inst. fuer Experimentelle Stroemungsmechanik

January 1984

SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...

Experiments in a three-dimensional adaptive-wall wind tunnel /

Schairer, Edward T.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."September 1983"--Cover.Includes bibliographical r...

Adaptive wall technology for two-dimensional wind tunnel testing at high subsonic through to low supersonic speeds

Taylor, N.J

January 1995

SIGLEAvailable from British Library Document Supply Centre-DSC:DX189107 / BLDSC - British Library Do...

Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic tunnel /

Mineck, Raymond E.
Hill, Acquilla S.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 8-9.Mode of access: Internet

A method for the design of porous-wall wind tunnels /

Stokes, George M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"January 20, 1956."Includes bibliographical references (p. 36).Mode of access: Internet

Turbulent wall jet in a coflowing stream /

Campbell, James F. (James Franklin), 1941-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-19).Mode ...

Reduction of wind-tunnel wall interference by controlled wall flow /

Bernstein, Samuel.
Joppa, Robert G. (Robert Glenn)
University of Washington. Dept. of Aeronautics and Astronautics.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 47-49).Mode of access: Internet

Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques /

Mineck, Raymond E.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 11).Mode of access: Inte...

Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels /

Green, Lawrence L. (Lawrence Lee)
Newman, Perry A.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 18.Mode of access: Internet

Aerofoil testing in a self-streamlining flexible walled wind tunnel /

Lewis, Mark Charles.
Langley Research Center.

January 1988

"May 1988"--Cover."Prepared for Langley Research Center under Grant NSG-7172."Includes bibliographic...

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section /

Mineck, Raymond E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1987

"December 1987"--Cover.Includes bibliographical references (p. 6).Mode of access: Internet

Wind tunnel interference factors for high-lift wings in closed wind tunnels /

Joppa, Robert G. (Robert Glenn)
Langley Research Center.
University of Washington.

"February 1973.""Prepared by University of Washington ... for Langley Research Center."Cover title.I...

Low-speed upwash interference on a transport model in a rectangular slotted-wall wind tunnel /

Mann, Michael J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Support interference of wind tunnel models : a selective annotated bibliography /

Tuttle, Marie H.
Gloss, Blair B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject category 09."March 1981"--Cover."Langley Research Center."Includes bibliographical reference...

Adaptive wall wind tunnels and wall interference correction methods

Hornung, H.
Stanewsky, E. (eds.)
Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt e.V., Goettingen (Germany, F.R.). Inst. fuer Experimentelle Stroemungsmechanik

January 1984

SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...

Experiments in a three-dimensional adaptive-wall wind tunnel /

Schairer, Edward T.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."September 1983"--Cover.Includes bibliographical r...

Adaptive wall technology for two-dimensional wind tunnel testing at high subsonic through to low supersonic speeds

Taylor, N.J

January 1995

SIGLEAvailable from British Library Document Supply Centre-DSC:DX189107 / BLDSC - British Library Do...

Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic tunnel /

Mineck, Raymond E.
Hill, Acquilla S.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 8-9.Mode of access: Internet

A method for the design of porous-wall wind tunnels /

Stokes, George M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"January 20, 1956."Includes bibliographical references (p. 36).Mode of access: Internet

Turbulent wall jet in a coflowing stream /

Campbell, James F. (James Franklin), 1941-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-19).Mode ...

Adaptive wall technology for minimization of wall interferences in transonic wind tunnels /

Abstract

Extracted data

Adaptive wall technology for minimization of wall interferences in transonic wind tunnels /

Abstract

Extracted data

Topics

Related items

Topics

Related items