Real-time computer data system for the 40- by 80-foot wind-tunnel facility at Ames Research Center /

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

Real-time computer data system for the 40- by 80-foot wind tunnel facility at Ames Research Center

Cambra, J. M.
Tolari, G. P.

May 1975

The background material and operational concepts of a computer-based system for an operating wind tu...

Design and performance of the University of Michigan 6.6-inch hypersonic wind tunnel /

Amick, James L.
Langley Research Center.
University of Michigan.

January 1975

"Prepared by the University of Michigan ... for Langley Research Center."Cover title.Includes biblio...

Application of a PC-based, real-time, data-acquisition system in rotorcraft wind-tunnel testing /

Wilbur, Matthew L.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 10.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 an all flush orifice air data system for a large subsonic aircraft /

Larson, Terry J.
Siemers, Paul M.
Flechner, Stuart G.
Langley Research Center.
Hugh L. Dryden Flight Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"May 1980"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliographical...

Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack /

Larson, Terry J.
Ames Research Center.

Prepared at Ames Research Center."April 1987"--Cover.Includes bibliographical references (p. 22-23)....

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 ...

Results of full-scale wind tunnel tests on the H.126 jet flap aircraft /

Aiken, Thomas N.
Cook, Anthony, M.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 4.Mode of access: Internet

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

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...

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:...

4D area navigation system description and flight test results /

Lee, Homer Q.
Hardy, Gordon H.
Neuman, Frank.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 51).Mode of acc...

Wind tunnel simulation of full scale vortices /

Rorke, James B.
Moffitt, Robert C.
Langley Research Center.
United Aircraft Corporation. Sikorsky Aircraft Division.

January 1973

"Prepared by Sikorsky Aircraft Division, United Aircraft Corporation ... for Langley Research Center...

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

Real-time computer data system for the 40- by 80-foot wind tunnel facility at Ames Research Center

Cambra, J. M.
Tolari, G. P.

May 1975

The background material and operational concepts of a computer-based system for an operating wind tu...

Design and performance of the University of Michigan 6.6-inch hypersonic wind tunnel /

Amick, James L.
Langley Research Center.
University of Michigan.

January 1975

"Prepared by the University of Michigan ... for Langley Research Center."Cover title.Includes biblio...

Application of a PC-based, real-time, data-acquisition system in rotorcraft wind-tunnel testing /

Wilbur, Matthew L.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 10.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 an all flush orifice air data system for a large subsonic aircraft /

Larson, Terry J.
Siemers, Paul M.
Flechner, Stuart G.
Langley Research Center.
Hugh L. Dryden Flight Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"May 1980"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliographical...

Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack /

Larson, Terry J.
Ames Research Center.

Prepared at Ames Research Center."April 1987"--Cover.Includes bibliographical references (p. 22-23)....

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 ...

Results of full-scale wind tunnel tests on the H.126 jet flap aircraft /

Aiken, Thomas N.
Cook, Anthony, M.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 4.Mode of access: Internet

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

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...

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:...

4D area navigation system description and flight test results /

Lee, Homer Q.
Hardy, Gordon H.
Neuman, Frank.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 51).Mode of acc...

Wind tunnel simulation of full scale vortices /

Rorke, James B.
Moffitt, Robert C.
Langley Research Center.
United Aircraft Corporation. Sikorsky Aircraft Division.

January 1973

"Prepared by Sikorsky Aircraft Division, United Aircraft Corporation ... for Langley Research Center...

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

Real-time computer data system for the 40- by 80-foot wind tunnel facility at Ames Research Center

Cambra, J. M.
Tolari, G. P.

May 1975

The background material and operational concepts of a computer-based system for an operating wind tu...

Real-time computer data system for the 40- by 80-foot wind-tunnel facility at Ames Research Center /

Abstract

Extracted data

Real-time computer data system for the 40- by 80-foot wind-tunnel facility at Ames Research Center /

Abstract

Extracted data

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