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 /

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...

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....

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 ...

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...

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...

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...

Experimental evaluation of wall Mach number distributions of the octagonal test section proposed for NASA Lewis Research Center's altitude wind tunnel /

Harrington, Douglas E.
Corban, Robert R.
Burley, Richard 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...

Experimental evaluation of honeycomb/screen configurations and short contraction section for NASA Lewis Research Center's altitude wind tunnel /

Burley, Richard R.
Harrington, Douglas E.
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 aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing /

Byrdsong, Thomas A.
Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche.Chiefly tables."June 1983"--Cover."Supplement to N...

Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles /

Sleeman, William C.
Hohlweg, William C.
Langley Research Center.

January 1975

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

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 ...

Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode /

Lance, Michael B.
Stroub, Robert H.
Sung, Daniel Y.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 24.Mode of access: Internet

Gust generator for a supersonic wind tunnel /

Sanders, Bobby W.
Webb, John A.
Bishop, Allan R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

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

Tuttle, Marie H.
Lawing, Pierce L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 09.Includes index.Distributed to depository libraries in microfiche."May 1984"--Cov...

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...

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....

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 ...

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...

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...

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...

Experimental evaluation of wall Mach number distributions of the octagonal test section proposed for NASA Lewis Research Center's altitude wind tunnel /

Harrington, Douglas E.
Corban, Robert R.
Burley, Richard 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...

Experimental evaluation of honeycomb/screen configurations and short contraction section for NASA Lewis Research Center's altitude wind tunnel /

Burley, Richard R.
Harrington, Douglas E.
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 aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing /

Byrdsong, Thomas A.
Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche.Chiefly tables."June 1983"--Cover."Supplement to N...

Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles /

Sleeman, William C.
Hohlweg, William C.
Langley Research Center.

January 1975

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

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 ...

Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode /

Lance, Michael B.
Stroub, Robert H.
Sung, Daniel Y.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 24.Mode of access: Internet

Gust generator for a supersonic wind tunnel /

Sanders, Bobby W.
Webb, John A.
Bishop, Allan R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

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

Tuttle, Marie H.
Lawing, Pierce L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 09.Includes index.Distributed to depository libraries in microfiche."May 1984"--Cov...

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...

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....

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 ...

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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

Related items

Related items