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

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

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: ...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

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 location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport airplane /

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

January 1990

Prepared at Langley Research Center.Bibliography: p. 7-8.Mode of access: Internet

Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport /

Lamb, Milton.
Abeyounis, William Kelly.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986."Includes bibliographical references (p. 4).Mode of ...

Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing /

Lee, Edwin E.
Pendergraft, Odis C.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 2...

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

Nacelle/pylon/wing integration on a transport model with a natural laminar flow nacelle /

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

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4-5)....

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

Reubush, David E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

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...

Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement /

Henderson, William P.
Abeyounis, William Kelly.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1985

Distributed to depository libraries in microfiche.Chiefly ill."December 1985"--Cover.Bibliography: p...

Calculation of the longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations /

Mendenhall, Michael R.
Spangler, Selden B., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued Aug. 1978.Prepared for Langley Research Center, by Nielsen Engineering & Research, Inc., unde...

Calculation of aerodynamic characteristics of airplane configurations at high angles of attack /

Tseng, Jing-Biau.
Lan, C. Edward (Chun-Tau Edward), 1935-
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Grant NAG1-635."Includes bibliogra...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

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: ...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

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 location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport airplane /

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

January 1990

Prepared at Langley Research Center.Bibliography: p. 7-8.Mode of access: Internet

Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport /

Lamb, Milton.
Abeyounis, William Kelly.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986."Includes bibliographical references (p. 4).Mode of ...

Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing /

Lee, Edwin E.
Pendergraft, Odis C.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 2...

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

Nacelle/pylon/wing integration on a transport model with a natural laminar flow nacelle /

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

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4-5)....

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

Reubush, David E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

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...

Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement /

Henderson, William P.
Abeyounis, William Kelly.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1985

Distributed to depository libraries in microfiche.Chiefly ill."December 1985"--Cover.Bibliography: p...

Calculation of the longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations /

Mendenhall, Michael R.
Spangler, Selden B., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued Aug. 1978.Prepared for Langley Research Center, by Nielsen Engineering & Research, Inc., unde...

Calculation of aerodynamic characteristics of airplane configurations at high angles of attack /

Tseng, Jing-Biau.
Lan, C. Edward (Chun-Tau Edward), 1935-
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Grant NAG1-635."Includes bibliogra...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

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: ...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

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

Abstract

Extracted data

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

Abstract

Extracted data

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