Simulator study of the stall departure characteristics of a light general aviation airplane with and without a wing-leading-edge modification /

Simulator study of minimum acceptable level of longitudinal stability for a representative STOL configuration during landing approach /

Grantham, William D.
Deal, Perry L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).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...

Fixed-base simulation study of decoupled longitudinal controls during approach and landing of a medium jet transport in the presence of wind shear /

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

January 1979

Subject Category 08."October 1979"--Cover."Langley Research Center."Includes bibliographical referen...

Simulator study of flight characteristics of several large dissimilar, cargo transport airplanes during approach and landing /

Grantham, William D.
Langley Research Center.

January 1984

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 1...

Simulator study of stall/post-stall characteristics of a fighter airplane with longitudinal static stability /

Nguyen, Luat T.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

Piloted simulation study of the effects of an automatic trim system on flight characteristics of a light twin-engine airplane with one engine inoperative /

Stewart, Eric C.
Yenni, Kenneth R.
Brown, Philip W.
Langley Research Center.

January 1986

Prepared at Langley Research Center."November 1986"--Cover.Includes bibliographical references (p. 1...

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...

Flight investigation of stall, spin, and recovery 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 1985

"May 1985"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. 8).Mod...

Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane /

Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 05."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane /

Grantham, William D.
Deal, Perry L.
Nguyen, Luat T.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

A piloted fixed-base simulator study of low-speed flight characteristics of an arrow-wing supersonic transport design /

Grantham, William D.
Deal, Perry L.
Langley Research Center.

Prepared at Langley Research Center."January 1968"--Cover.Includes bibliographical references (p. 17...

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:...

Effect of Reynolds number and engine nacelles on the stalling characteristics of a model of a twin-engine light airplane /

Lockwood, Vernard E.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

A piloted simulation study of operational aspects of the stall pitch-up /

White, Maurice D.
Cooper, George E.
Ames Research Center.

Prepared at Ames Research Center."July 1967"--Cover.Includes bibliographical references (p. 13).Mode...

A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise /

Grantham, William D.
Deal, Perry L.
Smith, Paul M., 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

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

Simulator study of minimum acceptable level of longitudinal stability for a representative STOL configuration during landing approach /

Grantham, William D.
Deal, Perry L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).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...

Fixed-base simulation study of decoupled longitudinal controls during approach and landing of a medium jet transport in the presence of wind shear /

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

January 1979

Subject Category 08."October 1979"--Cover."Langley Research Center."Includes bibliographical referen...

Simulator study of flight characteristics of several large dissimilar, cargo transport airplanes during approach and landing /

Grantham, William D.
Langley Research Center.

January 1984

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 1...

Simulator study of stall/post-stall characteristics of a fighter airplane with longitudinal static stability /

Nguyen, Luat T.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

Piloted simulation study of the effects of an automatic trim system on flight characteristics of a light twin-engine airplane with one engine inoperative /

Stewart, Eric C.
Yenni, Kenneth R.
Brown, Philip W.
Langley Research Center.

January 1986

Prepared at Langley Research Center."November 1986"--Cover.Includes bibliographical references (p. 1...

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...

Flight investigation of stall, spin, and recovery 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 1985

"May 1985"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. 8).Mod...

Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane /

Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 05."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane /

Grantham, William D.
Deal, Perry L.
Nguyen, Luat T.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

A piloted fixed-base simulator study of low-speed flight characteristics of an arrow-wing supersonic transport design /

Grantham, William D.
Deal, Perry L.
Langley Research Center.

Prepared at Langley Research Center."January 1968"--Cover.Includes bibliographical references (p. 17...

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:...

Effect of Reynolds number and engine nacelles on the stalling characteristics of a model of a twin-engine light airplane /

Lockwood, Vernard E.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

A piloted simulation study of operational aspects of the stall pitch-up /

White, Maurice D.
Cooper, George E.
Ames Research Center.

Prepared at Ames Research Center."July 1967"--Cover.Includes bibliographical references (p. 13).Mode...

A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise /

Grantham, William D.
Deal, Perry L.
Smith, Paul M., 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

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

Simulator study of minimum acceptable level of longitudinal stability for a representative STOL configuration during landing approach /

Grantham, William D.
Deal, Perry L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).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...

Fixed-base simulation study of decoupled longitudinal controls during approach and landing of a medium jet transport in the presence of wind shear /

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

January 1979

Subject Category 08."October 1979"--Cover."Langley Research Center."Includes bibliographical referen...

Simulator study of the stall departure characteristics of a light general aviation airplane with and without a wing-leading-edge modification /

Abstract

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Simulator study of the stall departure characteristics of a light general aviation airplane with and without a wing-leading-edge modification /

Abstract

Extracted data

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