Miniature flow-direction and airspeed sensor for airplanes and radio-controlled models in spin studies /

A celestial attitude measurement instrument for Project Scanner /

Walsh, T. M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1968

Prepared at Langley Research Center."August 1968"--Cover.Includes bibliographical references (p. 14)...

Operational evaluation of a propeller test stand in the quiet flow facility at Langley Research Center /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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:...

Spin tests of a single-engine, high-wing light airplane /

Stewart, Eric C.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject category 05."Langley Research Center.""January 1982"--Cover.Includes bibliographical referen...

Experiments in sensing transient rotational accelaration cues on a flight simulator /

Parrish, Russell V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

A low energy electron magnetometer /

Singh, Jag J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Langley Research Center.""December 1979"-- Cover.Includes bibliographical references.Mode of access...

Wind-tunnel investigation of an armed mini remotely piloted vehicle /

Phelps, Arthur E.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."September 1979"--Cover."Structures Laboratory, AVRADCOM Research and Technology...

Laser velocimeter systems analysis applied to a flow survey above a stalled wing /

Young, Warren H.
Hepner, Timothy E.
Meyers, James F.
Langley Directorate.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Aug. 1977."Langley Directorate, U.S. Army Air Mobility R&D Laboratory, Hampton, Va.""Langley Resear...

On the use of a magnetometer to determine the angular motion of a spinning body in regular precession /

Young, George R.
Timmons, Jesse D.
Langley Research Center.

Prepared at Langley Research Center."May 1964"--Cover.Includes bibliographical references (p. 13.Mod...

Accuracy of aircraft velocities obtained from inertial navigation systems for application to airborne wind measurements /

Rhyne, Richard H.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"July 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

Flight test of a pitch control for a spinning vehicle /

Garner, H. Douglas.
Reid, H. J. E.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Light airplane crash tests at three roll angles /

Castle, Claude B.
Alfaro-Bou, Emilio.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

A scanning laser-velocimeter technique for measuring two-dimensional wake-vortex velocity distributions /

Gartrell, Luther R.
Rhodes, David B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""May 1980"--Cover.Includes bibliographical references.Mode of access: Inte...

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 (...

A celestial attitude measurement instrument for Project Scanner /

Walsh, T. M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1968

Prepared at Langley Research Center."August 1968"--Cover.Includes bibliographical references (p. 14)...

Operational evaluation of a propeller test stand in the quiet flow facility at Langley Research Center /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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:...

Spin tests of a single-engine, high-wing light airplane /

Stewart, Eric C.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject category 05."Langley Research Center.""January 1982"--Cover.Includes bibliographical referen...

Experiments in sensing transient rotational accelaration cues on a flight simulator /

Parrish, Russell V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

A low energy electron magnetometer /

Singh, Jag J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Langley Research Center.""December 1979"-- Cover.Includes bibliographical references.Mode of access...

Wind-tunnel investigation of an armed mini remotely piloted vehicle /

Phelps, Arthur E.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."September 1979"--Cover."Structures Laboratory, AVRADCOM Research and Technology...

Laser velocimeter systems analysis applied to a flow survey above a stalled wing /

Young, Warren H.
Hepner, Timothy E.
Meyers, James F.
Langley Directorate.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Aug. 1977."Langley Directorate, U.S. Army Air Mobility R&D Laboratory, Hampton, Va.""Langley Resear...

On the use of a magnetometer to determine the angular motion of a spinning body in regular precession /

Young, George R.
Timmons, Jesse D.
Langley Research Center.

Prepared at Langley Research Center."May 1964"--Cover.Includes bibliographical references (p. 13.Mod...

Accuracy of aircraft velocities obtained from inertial navigation systems for application to airborne wind measurements /

Rhyne, Richard H.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"July 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

Flight test of a pitch control for a spinning vehicle /

Garner, H. Douglas.
Reid, H. J. E.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Light airplane crash tests at three roll angles /

Castle, Claude B.
Alfaro-Bou, Emilio.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

A scanning laser-velocimeter technique for measuring two-dimensional wake-vortex velocity distributions /

Gartrell, Luther R.
Rhodes, David B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""May 1980"--Cover.Includes bibliographical references.Mode of access: Inte...

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 (...

A celestial attitude measurement instrument for Project Scanner /

Walsh, T. M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1968

Prepared at Langley Research Center."August 1968"--Cover.Includes bibliographical references (p. 14)...

Operational evaluation of a propeller test stand in the quiet flow facility at Langley Research Center /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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:...

Miniature flow-direction and airspeed sensor for airplanes and radio-controlled models in spin studies /

Abstract

Extracted data

Miniature flow-direction and airspeed sensor for airplanes and radio-controlled models in spin studies /

Abstract

Extracted data

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