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

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...

An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds /

Carlson, John R.
Pendergraft, Odis C.
Langley Research Center.

January 1987

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

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration /

Harris, Charles D., 1952-
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 14-15).Mode of access: I...

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...

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)....

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...

Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds /

Covell, Peter F.
Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."April 1987"--Cover.Includes bibliographical references (p. 6-7)...

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:...

Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment /

Newman, Perry A.
Peterson, John B.
Anderson, E. Clay.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"September 1984"--Cover.Subject category 02.Distributed to depository libraries in microfiche.Includ...

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

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...

Technology for pressure-instrumented thin airfoil models /

Wigley, David A.
Langley Research Center.

January 1988

"September 1988"--Cover."Prepared for Langley Research Center under Contract NAS1-18066."Includes bi...

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...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

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...

An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds /

Carlson, John R.
Pendergraft, Odis C.
Langley Research Center.

January 1987

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

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration /

Harris, Charles D., 1952-
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 14-15).Mode of access: I...

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...

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)....

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...

Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds /

Covell, Peter F.
Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."April 1987"--Cover.Includes bibliographical references (p. 6-7)...

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:...

Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment /

Newman, Perry A.
Peterson, John B.
Anderson, E. Clay.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"September 1984"--Cover.Subject category 02.Distributed to depository libraries in microfiche.Includ...

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

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...

Technology for pressure-instrumented thin airfoil models /

Wigley, David A.
Langley Research Center.

January 1988

"September 1988"--Cover."Prepared for Langley Research Center under Contract NAS1-18066."Includes bi...

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...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

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...

An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds /

Carlson, John R.
Pendergraft, Odis C.
Langley Research Center.

January 1987

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

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

Abstract

Extracted data

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

Abstract

Extracted data

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