Effects of winglets on first-generation jet transport wing /

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 Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds /

Stallings, Robert L.
Watson, Carolyn B.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""July 1980"--Cover.Includes bibliographical references.Mode of access: Int...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

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...

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...

Effect of winglets on a first-generation jet transport wing.

Meyer, Robert R.
Langley Research Center.
United States. Air Force.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

The static longitudinal and lateral directional characteristics of a 0.035 scale model of a first ge...

Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag /

Kuhlmann, John, 1948-
Cerney, Michael J.
Liaw, Paul.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

Prepared for Langley Research Center under Grant NAG1-625."August 1988"--Cover.Bibliography: p. 34-3...

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...

Effect of leading-edge load constraints on the design and performance of supersonic wings /

Darden, Christine M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 7).Mo...

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...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

Re, Richard J.
Reubush, David E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

The Influence of wing loading on turbofan powered STOL transports with and without externally blown flaps /

Morris, R. L.
Langley Research Center.
Boeing Company. Wichita Division.

January 1973

"Prepared by the Boeing Company, Wichita Division, ... for Langley Research Center."Cover title.Bibl...

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

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 Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds /

Stallings, Robert L.
Watson, Carolyn B.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""July 1980"--Cover.Includes bibliographical references.Mode of access: Int...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

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...

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...

Effect of winglets on a first-generation jet transport wing.

Meyer, Robert R.
Langley Research Center.
United States. Air Force.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

The static longitudinal and lateral directional characteristics of a 0.035 scale model of a first ge...

Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag /

Kuhlmann, John, 1948-
Cerney, Michael J.
Liaw, Paul.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

Prepared for Langley Research Center under Grant NAG1-625."August 1988"--Cover.Bibliography: p. 34-3...

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...

Effect of leading-edge load constraints on the design and performance of supersonic wings /

Darden, Christine M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 7).Mo...

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...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

Re, Richard J.
Reubush, David E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

The Influence of wing loading on turbofan powered STOL transports with and without externally blown flaps /

Morris, R. L.
Langley Research Center.
Boeing Company. Wichita Division.

January 1973

"Prepared by the Boeing Company, Wichita Division, ... for Langley Research Center."Cover title.Bibl...

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

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 Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds /

Stallings, Robert L.
Watson, Carolyn B.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""July 1980"--Cover.Includes bibliographical references.Mode of access: Int...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

Effects of winglets on first-generation jet transport wing /

Abstract

Extracted data

Effects of winglets on first-generation jet transport wing /

Abstract

Extracted data

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