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

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

Gartrell, L. R.
Rhodes, D. B.

May 1980

A rapid scanning two dimensional laser velocimeter (LV) has been used to measure simultaneously the ...

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

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Preliminary rotor wake measurements with a laser velocimeter /

Hoad, Danny R.
Rhodes, David B.
Meyers, James F.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"Langley Research Center."Subject category 34."March 1983"--Cover."Structures Laboratory, AVRADCOM R...

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...

Laser velocimetry technique applied to the Langley 0.3-Meter transonic cryogenic tunnel /

Gartrell, Luther R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Frequency domain laser velocimeter signal processor : a new signal processing scheme /

Meyers, James F.
Clemmons, James I.
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Measurement of velocity and vorticity fields in the wake of an airfoil in periodic pitching motion /

Booth, Earl R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."December 1987"--Cover.Includes bibliographical references (p. 7...

Laser velocimeter (autocovariance) buffer interface /

Clemmons, James I.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

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

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

Kershner, David D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

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

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

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...

Performance test of laser velocimeter system for the Langley 16-Foot Transonic Tunnel /

Meyers, James F.
United States. Army Aviation Systems Command. Aerostructures Directorate.
Langley Research Center.

January 1985

Prepared at Langley Research Center and Aerostructures Diectorate, USAARTA-AVSCOM."December 1985"--C...

Investigation of variation in base pressure over the Reynolds number range in which wake transition occurs for two-dimensional bodies at Mach numbers from 1.95 to 2.92 /

Van Hise, Vernon.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

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

Gartrell, L. R.
Rhodes, D. B.

May 1980

A rapid scanning two dimensional laser velocimeter (LV) has been used to measure simultaneously the ...

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

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Preliminary rotor wake measurements with a laser velocimeter /

Hoad, Danny R.
Rhodes, David B.
Meyers, James F.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"Langley Research Center."Subject category 34."March 1983"--Cover."Structures Laboratory, AVRADCOM R...

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...

Laser velocimetry technique applied to the Langley 0.3-Meter transonic cryogenic tunnel /

Gartrell, Luther R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Frequency domain laser velocimeter signal processor : a new signal processing scheme /

Meyers, James F.
Clemmons, James I.
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Measurement of velocity and vorticity fields in the wake of an airfoil in periodic pitching motion /

Booth, Earl R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."December 1987"--Cover.Includes bibliographical references (p. 7...

Laser velocimeter (autocovariance) buffer interface /

Clemmons, James I.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

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

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

Kershner, David D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

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

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

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...

Performance test of laser velocimeter system for the Langley 16-Foot Transonic Tunnel /

Meyers, James F.
United States. Army Aviation Systems Command. Aerostructures Directorate.
Langley Research Center.

January 1985

Prepared at Langley Research Center and Aerostructures Diectorate, USAARTA-AVSCOM."December 1985"--C...

Investigation of variation in base pressure over the Reynolds number range in which wake transition occurs for two-dimensional bodies at Mach numbers from 1.95 to 2.92 /

Van Hise, Vernon.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

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

Gartrell, L. R.
Rhodes, D. B.

May 1980

A rapid scanning two dimensional laser velocimeter (LV) has been used to measure simultaneously the ...

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

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

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

Abstract

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

Abstract

Extracted data

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