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

Streamline curvature design procedure for subsonic and transonic ducts /

Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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 ...

Calculated wind-tunnel-boundary lift-interference factors for rectangular perforated test sections /

Schilling, Benferd L.
Wright, Ray H.
Langley Research Center.

Prepared at Langley Research Center."January 1970."Cover title.Includes bibliographical references (...

Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models /

Wright, Ray H.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Prepared at Langley Research Center.N68 31592.Includes bibliographical references (p. 84-84).Mode of...

Rapid estimation of wind-tunnel corrections with application to wind-tunnel and model design /

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

January 1971

Prepared at Langley Research Center.N71-36675.Includes bibliographical references (p. 48-50).Mode of...

Experimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel /

Moore, Royce D.
Shyne, Rickey J.
Boldman, Donald R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1986

Distributed to depository libraries in microfiche.Includes bibliographical references.Mode of access...

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /

Hallissy, James B.
Phillips, Pamela S.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 5-6.Mode of access: Internet

Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel /

Boldman, Donald R.
Shyne, Rickey J.
Moore, Royce D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1987

Distributed to depository libraries in microfiche.Includes bibliographical references.Mode of access...

Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects /

Gentry, Garl L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Chiefly graphs.Cover title.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....

Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel /

Moore, Royce D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1987

Distributed to depository libraries in microfiche.Includes bibliographical references.Mode of access...

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...

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel /

Gelder, Thomas F.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1987

Distributed to depository libraries in microfiche.Includes bibliographical references.Mode of access...

Streamline curvature design procedure for subsonic and transonic ducts /

Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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 ...

Calculated wind-tunnel-boundary lift-interference factors for rectangular perforated test sections /

Schilling, Benferd L.
Wright, Ray H.
Langley Research Center.

Prepared at Langley Research Center."January 1970."Cover title.Includes bibliographical references (...

Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models /

Wright, Ray H.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Prepared at Langley Research Center.N68 31592.Includes bibliographical references (p. 84-84).Mode of...

Rapid estimation of wind-tunnel corrections with application to wind-tunnel and model design /

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

January 1971

Prepared at Langley Research Center.N71-36675.Includes bibliographical references (p. 48-50).Mode of...

Experimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel /

Moore, Royce D.
Shyne, Rickey J.
Boldman, Donald R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1986

Distributed to depository libraries in microfiche.Includes bibliographical references.Mode of access...

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /

Hallissy, James B.
Phillips, Pamela S.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 5-6.Mode of access: Internet

Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel /

Boldman, Donald R.
Shyne, Rickey J.
Moore, Royce D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1987

Distributed to depository libraries in microfiche.Includes bibliographical references.Mode of access...

Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects /

Gentry, Garl L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Chiefly graphs.Cover title.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....

Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel /

Moore, Royce D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1987

Distributed to depository libraries in microfiche.Includes bibliographical references.Mode of access...

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...

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel /

Gelder, Thomas F.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1987

Distributed to depository libraries in microfiche.Includes bibliographical references.Mode of access...

Streamline curvature design procedure for subsonic and transonic ducts /

Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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 ...

Calculated wind-tunnel-boundary lift-interference factors for rectangular perforated test sections /

Schilling, Benferd L.
Wright, Ray H.
Langley Research Center.

Prepared at Langley Research Center."January 1970."Cover title.Includes bibliographical references (...

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

Abstract

Extracted data

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

Abstract

Extracted data

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