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

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

An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers /

McGowan, William A.
Langley Research Center.

January 1959

"NASA TN D-100.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

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...

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

Hindson, W. S.
Innis, Robert C.
Hardy, Gordon H.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"March 1981"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Inter...

Evaluation of advanced lift concepts and potential fuel conservation for short-haul aircraft /

Sweet, H. S.
Bowden, M. K.
Renshaw, J. H.
Ames Research Center.
Lockheed Aircraft Corporation.

"Prepared by Lockheed Aircraft Corporation ... for Ames Research Center.""February 1975."Cover title...

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 ...

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 ...

Planning fuel-conservative descents in an airline environment using a small programmable calculator : algorithm development and flight test results /

Knox, Charles E.
Simmon, David A.
Vicroy, Dan D.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 56).Mo...

Approximate solutions to optimum flight trajectories for a turbojet-powered aircraft /

Miele, Angelo.
Cappellari, James O.
Purdue University.

Prepared at Purdue University."September 1959."Cover title.Includes bibliographical references (p. 2...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Approach and landing investigation at lift-drag ratios of 2 to 4 utilizing a straight-wing fighter airplane /

Matranga, Gene J.
Armstrong, Neil, 1930-
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Analysis of a theoretically optimized transonic airfoil /

Lores, M. E.
Shrewsbury, George D., 1939-
Burdges, Kenneth P.
Ames Research Center.
Lockheed-Georgia Company.

January 1978

"Prepared [at Lockheed-Georgia Company] for Ames Research Center under Contract NAS2-8697.""November...

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)...

A computer technique for detailed analysis of mission radius and maneuverability characteristics of fighter aircraft /

Foss, Willard E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

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

An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers /

McGowan, William A.
Langley Research Center.

January 1959

"NASA TN D-100.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

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...

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

Hindson, W. S.
Innis, Robert C.
Hardy, Gordon H.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"March 1981"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Inter...

Evaluation of advanced lift concepts and potential fuel conservation for short-haul aircraft /

Sweet, H. S.
Bowden, M. K.
Renshaw, J. H.
Ames Research Center.
Lockheed Aircraft Corporation.

"Prepared by Lockheed Aircraft Corporation ... for Ames Research Center.""February 1975."Cover title...

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 ...

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 ...

Planning fuel-conservative descents in an airline environment using a small programmable calculator : algorithm development and flight test results /

Knox, Charles E.
Simmon, David A.
Vicroy, Dan D.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 56).Mo...

Approximate solutions to optimum flight trajectories for a turbojet-powered aircraft /

Miele, Angelo.
Cappellari, James O.
Purdue University.

Prepared at Purdue University."September 1959."Cover title.Includes bibliographical references (p. 2...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Approach and landing investigation at lift-drag ratios of 2 to 4 utilizing a straight-wing fighter airplane /

Matranga, Gene J.
Armstrong, Neil, 1930-
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Analysis of a theoretically optimized transonic airfoil /

Lores, M. E.
Shrewsbury, George D., 1939-
Burdges, Kenneth P.
Ames Research Center.
Lockheed-Georgia Company.

January 1978

"Prepared [at Lockheed-Georgia Company] for Ames Research Center under Contract NAS2-8697.""November...

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)...

A computer technique for detailed analysis of mission radius and maneuverability characteristics of fighter aircraft /

Foss, Willard E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

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

An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers /

McGowan, William A.
Langley Research Center.

January 1959

"NASA TN D-100.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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