An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics /

Some effects of variations in density and aerodynamic parameters on the calculated flutter characteristics of finite-span swept and unswept wings at subsonic and supersonic speeds /

Yates, E. Carson (Edward Carson), 1926-
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 22-23).Mode of access: Internet

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

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)...

Effect of under-wing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane /

Abeyounis, William Kelly.
Patterson, James C.
Langley Research Center.

January 1985

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

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect /

Paulson, John W.
Kjelgaard, Scott O.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration /

Coe, Paul L.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references.Mode of access: Internet

An experimental investigation of nacelle-pylon installation on an unswept wing at subsonic and transonic speeds /

Carlson, John R.
Compton, William B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 02."February 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /

Lamb, Milton.
Pendergraft, Odis C.
Carlson, John R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1987

"November 1987"--Cover.Includes bibliographical references (p. 3).Mode of access: Internet

Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration /

Mann, Michael J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane /

Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 05."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor /

Yates, E. Carson.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

Some effects of variations in density and aerodynamic parameters on the calculated flutter characteristics of finite-span swept and unswept wings at subsonic and supersonic speeds /

Yates, E. Carson (Edward Carson), 1926-
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 22-23).Mode of access: Internet

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

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)...

Effect of under-wing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane /

Abeyounis, William Kelly.
Patterson, James C.
Langley Research Center.

January 1985

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

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect /

Paulson, John W.
Kjelgaard, Scott O.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration /

Coe, Paul L.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references.Mode of access: Internet

An experimental investigation of nacelle-pylon installation on an unswept wing at subsonic and transonic speeds /

Carlson, John R.
Compton, William B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 02."February 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /

Lamb, Milton.
Pendergraft, Odis C.
Carlson, John R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1987

"November 1987"--Cover.Includes bibliographical references (p. 3).Mode of access: Internet

Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration /

Mann, Michael J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane /

Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 05."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor /

Yates, E. Carson.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

Some effects of variations in density and aerodynamic parameters on the calculated flutter characteristics of finite-span swept and unswept wings at subsonic and supersonic speeds /

Yates, E. Carson (Edward Carson), 1926-
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 22-23).Mode of access: Internet

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

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)...

An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics /

Abstract

Extracted data

An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics /

Abstract

Extracted data

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