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

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...

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...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

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

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...

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 ...

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

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...

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...

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...

Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane /

Stough, H. Paul.
Patton, James M., Jr.
DiCarlo, Daniel J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 9).Mo...

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)....

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...

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: ...

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...

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...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

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

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...

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 ...

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

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...

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...

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...

Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane /

Stough, H. Paul.
Patton, James M., Jr.
DiCarlo, Daniel J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 9).Mo...

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)....

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...

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: ...

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...

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...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

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

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

Abstract

Extracted data

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

Abstract

Extracted data

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