Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models /

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...

Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack /

Carr, Peter C.
Gilbert, William P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Hugh L. Dryden Flight Research Center.

January 1979

"December 1979"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliograp...

Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser /

Banks, Daniel W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

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: ...

Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes /

Satran, Dale R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

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...

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 afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds /

Bangert, Linda S.
Reubush, David E.
Leavitt, Laurence D.
Langley Research Center.

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 13).M...

Influence of base modifications on in-flight base drag in the presence of jet exhaust for Mach numbers from 0.7 to 1.5 /

Powers, Sheryll Goecke.
Ames Research Center.

January 1988

Prepared at Ames Research Center."February 1988"--Cover.Includes bibliographical references (p. 6).M...

Simulator evaluation of the effects of reduced spoiler and thrust authority on a decoupled longitudinal control system during landings in wind shear /

Miller, G. Kimball.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 08."October 1981"--Cover."Langley Research Center."Includes bibliographical referen...

Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers /

Pendergraft, Odis C.
Bare, E. Ann.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

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 a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 ̊sweptback wing at a Mach number of 0.30 /

Henderson, William P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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...

Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack /

Carr, Peter C.
Gilbert, William P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Hugh L. Dryden Flight Research Center.

January 1979

"December 1979"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliograp...

Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser /

Banks, Daniel W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

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: ...

Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes /

Satran, Dale R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

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...

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 afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds /

Bangert, Linda S.
Reubush, David E.
Leavitt, Laurence D.
Langley Research Center.

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 13).M...

Influence of base modifications on in-flight base drag in the presence of jet exhaust for Mach numbers from 0.7 to 1.5 /

Powers, Sheryll Goecke.
Ames Research Center.

January 1988

Prepared at Ames Research Center."February 1988"--Cover.Includes bibliographical references (p. 6).M...

Simulator evaluation of the effects of reduced spoiler and thrust authority on a decoupled longitudinal control system during landings in wind shear /

Miller, G. Kimball.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 08."October 1981"--Cover."Langley Research Center."Includes bibliographical referen...

Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers /

Pendergraft, Odis C.
Bare, E. Ann.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

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 a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 ̊sweptback wing at a Mach number of 0.30 /

Henderson, William P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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...

Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack /

Carr, Peter C.
Gilbert, William P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Hugh L. Dryden Flight Research Center.

January 1979

"December 1979"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliograp...

Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser /

Banks, Daniel W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models /

Abstract

Extracted data

Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models /

Abstract

Extracted data

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