Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Section data for thin, highly cambered airfoils in incompressible flow /

Milgram, Jerome H.
Langley Research Center.
Massachusetts Institute of Technology.
United States. National Aeronautics and Space Administration.

"Prepared by Massachusetts Institute of Technology ... for Langley Research Center.""July 1971."Cove...

Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results /

Redd, L. Tracy.
Wynne, Eleanor C.
Hanson, Perry W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

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

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 (...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

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...

Wind-tunnel experiments on divergence of forward-swept wings /

Ricketts, Rodney H.
Doggett, Robert V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 05."August 1980"--Cover."Langley Research Center."Includes bibliographical referenc...

Aerofoil testing in a self-streamlining flexible walled wind tunnel /

Lewis, Mark Charles.
Langley Research Center.

January 1988

"May 1988"--Cover."Prepared for Langley Research Center under Grant NSG-7172."Includes bibliographic...

Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley low-turbulence pressure tunnel /

McGhee, Robert J.
Millard, Betty F.
Walker, Betty S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 228).Mode of access: Internet

Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes /

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

January 1981

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

Description and calibration of the Langley Unitary Plan Wind Tunnel /

Jackson, Charlie M.
Monta, William J.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel /

Hall, Robert M.
Langley Research Center.

Prepared at Langley Research Center."January 1986"--Cover.Includes bibliographical references (p. 11...

Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel /

Campbell, Richard L. (Richard Lawson), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

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....

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Section data for thin, highly cambered airfoils in incompressible flow /

Milgram, Jerome H.
Langley Research Center.
Massachusetts Institute of Technology.
United States. National Aeronautics and Space Administration.

"Prepared by Massachusetts Institute of Technology ... for Langley Research Center.""July 1971."Cove...

Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results /

Redd, L. Tracy.
Wynne, Eleanor C.
Hanson, Perry W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

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

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 (...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

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...

Wind-tunnel experiments on divergence of forward-swept wings /

Ricketts, Rodney H.
Doggett, Robert V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 05."August 1980"--Cover."Langley Research Center."Includes bibliographical referenc...

Aerofoil testing in a self-streamlining flexible walled wind tunnel /

Lewis, Mark Charles.
Langley Research Center.

January 1988

"May 1988"--Cover."Prepared for Langley Research Center under Grant NSG-7172."Includes bibliographic...

Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley low-turbulence pressure tunnel /

McGhee, Robert J.
Millard, Betty F.
Walker, Betty S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 228).Mode of access: Internet

Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes /

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

January 1981

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

Description and calibration of the Langley Unitary Plan Wind Tunnel /

Jackson, Charlie M.
Monta, William J.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel /

Hall, Robert M.
Langley Research Center.

Prepared at Langley Research Center."January 1986"--Cover.Includes bibliographical references (p. 11...

Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel /

Campbell, Richard L. (Richard Lawson), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

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....

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Section data for thin, highly cambered airfoils in incompressible flow /

Milgram, Jerome H.
Langley Research Center.
Massachusetts Institute of Technology.
United States. National Aeronautics and Space Administration.

"Prepared by Massachusetts Institute of Technology ... for Langley Research Center.""July 1971."Cove...

Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results /

Redd, L. Tracy.
Wynne, Eleanor C.
Hanson, Perry W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

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

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

Abstract

Extracted data

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

Abstract

Extracted data

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