An investigation of a direct side-force maneuvering system on a deflected jet VTOL aircraft /

Investigation of lateral stability at stall.

Bull, Gifford.

January 1954

"Aeronautical Research Laboratory. Contract no. AF 33(038)-10480, RDO no. 472-106."Mode of access: I...

An investigation of a two-dimensional propulsive lifting system /

Shollenberger, Carl A.
Ames Research Center.
California Institute of Technology.

January 1973

"Prepared by California Institute of Technology ... for Ames Research Center."Cover title.Bibliograp...

An experimental study of the effect of downwash from a twin-propeller VTOL aircraft on several types of ground surfaces /

O'Bryan, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Piloting.Includes bibliographical reference...

Results of a brief flight investigation of a coin-type STOL aircraft /

Feistel, Terrell W.
Innis, Robert C.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

"August 1967."Work performed at Ames Research Center.Includes bibliographical references (p. 14).Mod...

Technique for measuring side forces on a banked aircraft with a free-swiveling nose gear /

Stubbs, Sandy M.
Tanner, John A.

January 1986

Prepared at Langley Research Center."August 1986."Includes bibliographical references (p. 3).Mode of...

A flight and simulator study of directional augmentation criteria for a four-propellered STOL airplane /

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

Work performed at Ames Research Center.Includes bibliographical references (p. 20).NASA technical no...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

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...

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

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...

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...

Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle /

Mason, Mary L.
Asbury, Scott C.
Capone, Francis J.
Langley Research Center.

January 1992

Prepared at Langley Research Center."June 1992"--Cover.Includes bibliographical references (p. 9).Mo...

Investigation of lateral stability at stall.

Bull, Gifford.

January 1954

"Aeronautical Research Laboratory. Contract no. AF 33(038)-10480, RDO no. 472-106."Mode of access: I...

An investigation of a two-dimensional propulsive lifting system /

Shollenberger, Carl A.
Ames Research Center.
California Institute of Technology.

January 1973

"Prepared by California Institute of Technology ... for Ames Research Center."Cover title.Bibliograp...

An experimental study of the effect of downwash from a twin-propeller VTOL aircraft on several types of ground surfaces /

O'Bryan, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Piloting.Includes bibliographical reference...

Results of a brief flight investigation of a coin-type STOL aircraft /

Feistel, Terrell W.
Innis, Robert C.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

"August 1967."Work performed at Ames Research Center.Includes bibliographical references (p. 14).Mod...

Technique for measuring side forces on a banked aircraft with a free-swiveling nose gear /

Stubbs, Sandy M.
Tanner, John A.

January 1986

Prepared at Langley Research Center."August 1986."Includes bibliographical references (p. 3).Mode of...

A flight and simulator study of directional augmentation criteria for a four-propellered STOL airplane /

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

Work performed at Ames Research Center.Includes bibliographical references (p. 20).NASA technical no...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

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...

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

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...

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...

Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle /

Mason, Mary L.
Asbury, Scott C.
Capone, Francis J.
Langley Research Center.

January 1992

Prepared at Langley Research Center."June 1992"--Cover.Includes bibliographical references (p. 9).Mo...

Investigation of lateral stability at stall.

Bull, Gifford.

January 1954

"Aeronautical Research Laboratory. Contract no. AF 33(038)-10480, RDO no. 472-106."Mode of access: I...

An investigation of a two-dimensional propulsive lifting system /

Shollenberger, Carl A.
Ames Research Center.
California Institute of Technology.

January 1973

"Prepared by California Institute of Technology ... for Ames Research Center."Cover title.Bibliograp...

An experimental study of the effect of downwash from a twin-propeller VTOL aircraft on several types of ground surfaces /

O'Bryan, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Piloting.Includes bibliographical reference...

An investigation of a direct side-force maneuvering system on a deflected jet VTOL aircraft /

Abstract

Extracted data

An investigation of a direct side-force maneuvering system on a deflected jet VTOL aircraft /

Abstract

Extracted data

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