Lateral control characteristics of a powered model of a twin-propeller deflected slipstream STOL airplane configuration

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Aerodynamic characteristics of a large-scale V/STOL transport model with left and lift-cruise fans /

Hall, Leo P.
Kirk, Jerry V.
Hickey, David H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Lateral stability and control characteristics of a four-propleer deflected-slipstream VTOL model inculding the effects of ground proximity /

Kuhn, Richard E.
Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

Some flight characteristics of a deflected slipstream V/STOL aircraft /

Turner, Howard L.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range /

Vogler, Raymond D.
Kuhn, Richard E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"May 1965."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Transition and hovering flight characteristics of a tilt-duct VTOL research aircraft /

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

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Aerodynamic characteristics of four-duct tandem VTOL-aircraft configurations /

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

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Aerodynamic characteristics of a four-propeller tilt-wing VTOL model with twin vertical tails, including effects of ground proximity /

Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographica...

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

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...

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails /

Draper, John W.
Rose, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 15, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 /

Driver, Cornelius.
Spearman, M. Leroy.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

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

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Aerodynamic characteristics of a large-scale V/STOL transport model with left and lift-cruise fans /

Hall, Leo P.
Kirk, Jerry V.
Hickey, David H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Lateral stability and control characteristics of a four-propleer deflected-slipstream VTOL model inculding the effects of ground proximity /

Kuhn, Richard E.
Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

Some flight characteristics of a deflected slipstream V/STOL aircraft /

Turner, Howard L.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range /

Vogler, Raymond D.
Kuhn, Richard E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"May 1965."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Transition and hovering flight characteristics of a tilt-duct VTOL research aircraft /

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

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Aerodynamic characteristics of four-duct tandem VTOL-aircraft configurations /

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

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Aerodynamic characteristics of a four-propeller tilt-wing VTOL model with twin vertical tails, including effects of ground proximity /

Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographica...

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

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...

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails /

Draper, John W.
Rose, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 15, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 /

Driver, Cornelius.
Spearman, M. Leroy.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

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

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Aerodynamic characteristics of a large-scale V/STOL transport model with left and lift-cruise fans /

Hall, Leo P.
Kirk, Jerry V.
Hickey, David H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Lateral control characteristics of a powered model of a twin-propeller deflected slipstream STOL airplane configuration

Abstract

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Lateral control characteristics of a powered model of a twin-propeller deflected slipstream STOL airplane configuration

Abstract

Extracted data

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