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

The Cryogenic wind-tunnel concept for high Reynolds number testing /

Kilgore, Robert A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 53-55).Mode ...

Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels /

Heyson, Harry H.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N70-14133.Includes bibliographical references (p. 62-64).Mode of...

The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 /

Little, B. H.
Cubbage, James M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"May 10, 1955."Includes bibliographical references (p. 26-27).Mode of access: Internet

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

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

Wolf, Stephen W. D.
Langley Research Center.

January 1988

"November 1988"--Cover."Prepared for Langley Research Center under Contract NAS1-17919."Includes bib...

An experimental investigation of the transonic-flow-generation and shock-wave-reflection characteristics of a two-dimensional wind tunnel with 17-percent-open perforated walls /

Davis, Don D.
Stokes, George M.
Sellers, Thomas B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"April 26, 1954."Includes bibliographical references (p. 19).Mode of access: Internet

Experimental aerodynamics,

Pavian, Henry Christensen, 1907-
Michel, Phillip Lincoln.

"New York university nine-foot wind tunnel; manual by Phillip L. Michel (May 1939)": p. 143-164.Bibl...

A Numerical simulation of three-dimensional flow in an adaptive wall wind tunnel /

Mendoza, J. P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"August 1984."Distributed to depository libraries in microfiche.Includes bibliographical references....

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow /

Runyan, Harry L.
Rainey, A. Gerald.
Woolston, Donald S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 23, 1953."Includes bibliographical references (p. 24).Mode of access: Internet

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...

An investigation of a device to oscillate a wind-tunnel airstream /

Reid, Charles F.
Wrestler, Clifton, G.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Research and development facilities.Includes bibliographical references.Mod...

Tests of submerged duct installation on a modified fighter airplane in the Ames 40- by 80-foot wind tunnel /

Martin, Norman J.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "December 11, 1947."Includes bibliographical references: p. 7.Mode of access: Intern...

A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds /

Howell, Robert R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 24, 1954."Includes bibliographical references (p. 13).Mode of access: Internet

Flow visualization techniques for use in hypersonic wind tunnels /

Rhudy, R. W., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

"October 1964."Includes bibliograqphic references (page 8).Report prepared by ARO, Inc., under Air F...

The Cryogenic wind-tunnel concept for high Reynolds number testing /

Kilgore, Robert A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 53-55).Mode ...

Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels /

Heyson, Harry H.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N70-14133.Includes bibliographical references (p. 62-64).Mode of...

The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 /

Little, B. H.
Cubbage, James M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"May 10, 1955."Includes bibliographical references (p. 26-27).Mode of access: Internet

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

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

Wolf, Stephen W. D.
Langley Research Center.

January 1988

"November 1988"--Cover."Prepared for Langley Research Center under Contract NAS1-17919."Includes bib...

An experimental investigation of the transonic-flow-generation and shock-wave-reflection characteristics of a two-dimensional wind tunnel with 17-percent-open perforated walls /

Davis, Don D.
Stokes, George M.
Sellers, Thomas B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"April 26, 1954."Includes bibliographical references (p. 19).Mode of access: Internet

Experimental aerodynamics,

Pavian, Henry Christensen, 1907-
Michel, Phillip Lincoln.

"New York university nine-foot wind tunnel; manual by Phillip L. Michel (May 1939)": p. 143-164.Bibl...

A Numerical simulation of three-dimensional flow in an adaptive wall wind tunnel /

Mendoza, J. P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"August 1984."Distributed to depository libraries in microfiche.Includes bibliographical references....

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow /

Runyan, Harry L.
Rainey, A. Gerald.
Woolston, Donald S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 23, 1953."Includes bibliographical references (p. 24).Mode of access: Internet

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...

An investigation of a device to oscillate a wind-tunnel airstream /

Reid, Charles F.
Wrestler, Clifton, G.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Research and development facilities.Includes bibliographical references.Mod...

Tests of submerged duct installation on a modified fighter airplane in the Ames 40- by 80-foot wind tunnel /

Martin, Norman J.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "December 11, 1947."Includes bibliographical references: p. 7.Mode of access: Intern...

A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds /

Howell, Robert R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 24, 1954."Includes bibliographical references (p. 13).Mode of access: Internet

Flow visualization techniques for use in hypersonic wind tunnels /

Rhudy, R. W., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

"October 1964."Includes bibliograqphic references (page 8).Report prepared by ARO, Inc., under Air F...

The Cryogenic wind-tunnel concept for high Reynolds number testing /

Kilgore, Robert A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 53-55).Mode ...

Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels /

Heyson, Harry H.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N70-14133.Includes bibliographical references (p. 62-64).Mode of...

The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 /

Little, B. H.
Cubbage, James M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"May 10, 1955."Includes bibliographical references (p. 26-27).Mode of access: Internet

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

Abstract

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

Abstract

Extracted data

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