Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches /

Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model /

Feistel, Terrell W.
Morelli, Joseph P.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Aeromechanics Laboratory, AVRADCOM Research and Technology Laboratories, Ames Re...

Free-flight investigation of the stability and control characteristics of a STOL model with an externally blown jet flap /

Parlett, Lysle P.
Phelps, Arthur E.
Emerling, Sandy J. (Sandy James)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-20).Mode ...

Flight test of the slide-slope track and flare-control laws for an automatic landing system for a powered-lift STOL airplane /

Watson, DeLamar M.
Warner, David N.
Hardy, Gordon H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"December 1983"--Cover.Subject category 08.Distributed to depository libraries in microfiche.Include...

Flight evaluation of stabilization and command augmentation system concepts and cockpit displays during approach and landing of a powered-lift STOL aircraft /

Franklin, James A.
Hardy, Gordon H.
Innis, Robert C.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Ames Research Center."Includes bibliographical references.Mode of access: Internet

Analysis of fuel-conservative curved decelerating approach trajectories for powered-lift and CTOL jet aircraft /

Neuman, Frank.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Inter...

Design criteria for flightpath and airspeed control for the approach and landing of STOL aircraft /

Franklin, James A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Ames Research Center.

January 1982

STAR category 08."March 1982"--Cover."Ames Research Center."Includes bibliographical references.Mode...

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

Development and flight test of an experimental maneuver autopilot for a highly maneuverable aircraft /

Duke, Eugene L.
Roncoli, Ralph B.
Jones, Frank P.
Ames Research Center.

January 1986

Prepared at Ames Research Center."September 1986"--Cover.Includes bibliographical references (p. 30)...

Flight tests under IFR with an STOL transport aircraft /

Innis, Robert C.
Gallant, Richard P.
Holzhauser, Curt A.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."December 1968"--Cover.Includes bibliographical references (p. 19)....

Hovering and transition flight tests of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode of ...

In-flight simulation study of decoupled longitudinal controls for the approach and landing of a STOL aircraft /

Feinreich, Benjamin.
Ellis, David R., joint author.
Seckel, Edward, 1921-2009, joint author.
Princeton University.
United States. National Aeronautics and Space Administration.

January 1977

Issued Apr. 1977.Prepared by Princeton University for Langley Research Center.Includes bibliographic...

A Piloted evaluation of an oblique-wing research aircraft motion simulation with decoupling control laws /

Kempel, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 26).Mode of access: Internet

A flight study of the conversion maneuver of a tilt-duct VTOL aircraft /

Tapscott, Robert J.
Kelley, Henry L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Dynamics of tilting proprotor aircraft in cruise flight /

Johnson, Wayne, 1946-
U.S. Army Air Mobility Research and Development Laboratory.
Ames Research Center.

January 1974

Prepared at Ames Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes ...

Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks /

Fry, Emmett B.
Gerdes, Ronald M.
Greif, Richard K.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Evaluation of six degrees of freedom motion simulator for Bell X-14A aircraft hovering characteristi...

Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model /

Feistel, Terrell W.
Morelli, Joseph P.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Aeromechanics Laboratory, AVRADCOM Research and Technology Laboratories, Ames Re...

Free-flight investigation of the stability and control characteristics of a STOL model with an externally blown jet flap /

Parlett, Lysle P.
Phelps, Arthur E.
Emerling, Sandy J. (Sandy James)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-20).Mode ...

Flight test of the slide-slope track and flare-control laws for an automatic landing system for a powered-lift STOL airplane /

Watson, DeLamar M.
Warner, David N.
Hardy, Gordon H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"December 1983"--Cover.Subject category 08.Distributed to depository libraries in microfiche.Include...

Flight evaluation of stabilization and command augmentation system concepts and cockpit displays during approach and landing of a powered-lift STOL aircraft /

Franklin, James A.
Hardy, Gordon H.
Innis, Robert C.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Ames Research Center."Includes bibliographical references.Mode of access: Internet

Analysis of fuel-conservative curved decelerating approach trajectories for powered-lift and CTOL jet aircraft /

Neuman, Frank.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Inter...

Design criteria for flightpath and airspeed control for the approach and landing of STOL aircraft /

Franklin, James A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Ames Research Center.

January 1982

STAR category 08."March 1982"--Cover."Ames Research Center."Includes bibliographical references.Mode...

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

Development and flight test of an experimental maneuver autopilot for a highly maneuverable aircraft /

Duke, Eugene L.
Roncoli, Ralph B.
Jones, Frank P.
Ames Research Center.

January 1986

Prepared at Ames Research Center."September 1986"--Cover.Includes bibliographical references (p. 30)...

Flight tests under IFR with an STOL transport aircraft /

Innis, Robert C.
Gallant, Richard P.
Holzhauser, Curt A.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."December 1968"--Cover.Includes bibliographical references (p. 19)....

Hovering and transition flight tests of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode of ...

In-flight simulation study of decoupled longitudinal controls for the approach and landing of a STOL aircraft /

Feinreich, Benjamin.
Ellis, David R., joint author.
Seckel, Edward, 1921-2009, joint author.
Princeton University.
United States. National Aeronautics and Space Administration.

January 1977

Issued Apr. 1977.Prepared by Princeton University for Langley Research Center.Includes bibliographic...

A Piloted evaluation of an oblique-wing research aircraft motion simulation with decoupling control laws /

Kempel, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 26).Mode of access: Internet

A flight study of the conversion maneuver of a tilt-duct VTOL aircraft /

Tapscott, Robert J.
Kelley, Henry L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Dynamics of tilting proprotor aircraft in cruise flight /

Johnson, Wayne, 1946-
U.S. Army Air Mobility Research and Development Laboratory.
Ames Research Center.

January 1974

Prepared at Ames Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes ...

Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks /

Fry, Emmett B.
Gerdes, Ronald M.
Greif, Richard K.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Evaluation of six degrees of freedom motion simulator for Bell X-14A aircraft hovering characteristi...

Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model /

Feistel, Terrell W.
Morelli, Joseph P.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Aeromechanics Laboratory, AVRADCOM Research and Technology Laboratories, Ames Re...

Free-flight investigation of the stability and control characteristics of a STOL model with an externally blown jet flap /

Parlett, Lysle P.
Phelps, Arthur E.
Emerling, Sandy J. (Sandy James)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-20).Mode ...

Flight test of the slide-slope track and flare-control laws for an automatic landing system for a powered-lift STOL airplane /

Watson, DeLamar M.
Warner, David N.
Hardy, Gordon H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"December 1983"--Cover.Subject category 08.Distributed to depository libraries in microfiche.Include...

Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches /

Abstract

Extracted data

Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches /

Abstract

Extracted data

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