Surface pressure measurements at two tips of a model helicopter rotor in hover /

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Hovering measurements for twin-rotor configurations with and without overlap /

Sweet, George E.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Propulsion systems, air-jet.Includes bibliograph...

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 ...

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model /

Althoff, Susan L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"September 1988"--Cover.Includes bibliographical references (p. 7-8).Mode of access: Internet

Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight /

Runyan, Harry L.
Tai, H. (Hsiang)
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Hovering characteristics of a rotor having an airfoil section designed for a utility type of helicopter y James P. Shivers and William J. Monahan.

Shivers, James P.
Monahan, William J.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

An analytical evaluation of airfoil sections for helicopter rotor applications /

Bingham, Gene J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

Measurements of the time-averaged and instantaneous induced velocities in the wake of a helicopter rotor hovering at high tip speeds /

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

Cover title."July 1960."Aircraft; Propulsion systems, air-jet.Includes bibliographical references.Mo...

Hover performance tests of full scale variable geometry rotors /

Rorke, James B.
United States. National Aeronautics and Space Administration.
Langley Research Center.
United Technologies Corporation.
U.S. Army Air Mobility Research and Development Laboratory.

January 1976

Cover title.Includes bibliographical references (p. 26-27).Mode of access: Internet

Helicopter main-rotor noise : determination of source contributions using scaled model data /

Brooks, Thomas F.
Marcolini, Michael A.
Jolly, J. Ralph.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"August 1988"--Cover.Includes bibliographical references (p. 12).Mode of access: Internet

Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes /

Berry, John D.
Mineck, Raymond E.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
United States. Army Aviation Research and Development Command.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."U.S. Army AVRADCOM"--Cover."Structures Laboratory, AVRADCOM Research and Technology Labor...

Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /

Shrout, Barrett L.
Collins, Ida K.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Subject category 02."May 1979"--Cover."Langley Research Center."Includes bibliographical references....

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Hovering measurements for twin-rotor configurations with and without overlap /

Sweet, George E.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Propulsion systems, air-jet.Includes bibliograph...

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 ...

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model /

Althoff, Susan L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"September 1988"--Cover.Includes bibliographical references (p. 7-8).Mode of access: Internet

Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight /

Runyan, Harry L.
Tai, H. (Hsiang)
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Hovering characteristics of a rotor having an airfoil section designed for a utility type of helicopter y James P. Shivers and William J. Monahan.

Shivers, James P.
Monahan, William J.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

An analytical evaluation of airfoil sections for helicopter rotor applications /

Bingham, Gene J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

Measurements of the time-averaged and instantaneous induced velocities in the wake of a helicopter rotor hovering at high tip speeds /

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

Cover title."July 1960."Aircraft; Propulsion systems, air-jet.Includes bibliographical references.Mo...

Hover performance tests of full scale variable geometry rotors /

Rorke, James B.
United States. National Aeronautics and Space Administration.
Langley Research Center.
United Technologies Corporation.
U.S. Army Air Mobility Research and Development Laboratory.

January 1976

Cover title.Includes bibliographical references (p. 26-27).Mode of access: Internet

Helicopter main-rotor noise : determination of source contributions using scaled model data /

Brooks, Thomas F.
Marcolini, Michael A.
Jolly, J. Ralph.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"August 1988"--Cover.Includes bibliographical references (p. 12).Mode of access: Internet

Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes /

Berry, John D.
Mineck, Raymond E.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
United States. Army Aviation Research and Development Command.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."U.S. Army AVRADCOM"--Cover."Structures Laboratory, AVRADCOM Research and Technology Labor...

Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /

Shrout, Barrett L.
Collins, Ida K.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Subject category 02."May 1979"--Cover."Langley Research Center."Includes bibliographical references....

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Hovering measurements for twin-rotor configurations with and without overlap /

Sweet, George E.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Propulsion systems, air-jet.Includes bibliograph...

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 ...

Surface pressure measurements at two tips of a model helicopter rotor in hover /

Abstract

Extracted data

Surface pressure measurements at two tips of a model helicopter rotor in hover /

Abstract

Extracted data

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