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

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

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).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...

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...

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 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 five-jet VTOL configuration in the transition speed range /

Margason, Richard J. (Richard John), 1936-
Gentry, Garl L., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Research prepared at Langley Research Center.N68-36081.Cover title.Includes bibliographical referenc...

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

Margason, Richard J.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."November 1964."Includes bibliographical references.Mode of access: Internet

Low-speed measurements of static and oscillatory lateral stability derivatives of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

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

Cover title."September 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

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...

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

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

Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds /

Osborne, Robert S.
Ware, George M.
United States. National Aeronautics and Space Administration.

"April 1963."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

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

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

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).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...

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...

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 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 five-jet VTOL configuration in the transition speed range /

Margason, Richard J. (Richard John), 1936-
Gentry, Garl L., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Research prepared at Langley Research Center.N68-36081.Cover title.Includes bibliographical referenc...

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

Margason, Richard J.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."November 1964."Includes bibliographical references.Mode of access: Internet

Low-speed measurements of static and oscillatory lateral stability derivatives of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

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

Cover title."September 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

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...

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

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

Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds /

Osborne, Robert S.
Ware, George M.
United States. National Aeronautics and Space Administration.

"April 1963."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

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

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

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

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

Abstract

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

Abstract

Extracted data

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