Technology for pressure-instrumented thin airfoil models /

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

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...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.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:...

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...

The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers /

Plentovich, Elizabeth B.
Langley Research Center.

January 1986

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

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...

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...

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...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

Aerothermal tests of quilted dome models on a flat plate at a Mach number of 6.5 /

Glass, Christopher E. (Christopher Earl), 1955-
Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 13-14)...

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview /

Harris, Charles D., 1952-
Brooks, Cuyler W.
Harvey, William D., 1934-
Langley Research Center.

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 22-24)...

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

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 modified Theodorsen [epsilon]-function airfoil design procedure /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

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...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.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:...

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...

The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers /

Plentovich, Elizabeth B.
Langley Research Center.

January 1986

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

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...

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...

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...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

Aerothermal tests of quilted dome models on a flat plate at a Mach number of 6.5 /

Glass, Christopher E. (Christopher Earl), 1955-
Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 13-14)...

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview /

Harris, Charles D., 1952-
Brooks, Cuyler W.
Harvey, William D., 1934-
Langley Research Center.

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 22-24)...

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

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 modified Theodorsen [epsilon]-function airfoil design procedure /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

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...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Technology for pressure-instrumented thin airfoil models /

Abstract

Extracted data

Technology for pressure-instrumented thin airfoil models /

Abstract

Extracted data

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