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 /

Aerodynamic characteristics of low-aspect-ratio wings in close proximity to the ground/

Fink, Marvin P.
Lastinger, James L.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and con...

Low-speed investigation of a full-span internal-flow jet-augmented flap on a high-wing model with a 35 degree swept wing of aspect ratio 7.0 /

Turner, Thomas R.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft, Aircraft; Stability and control.Includes bibliogra...

Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson.

Johnson, Joseph L.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogra...

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

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

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 canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond.

Spencer, Bernard.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Satellite...

Low-speed longitudinal characteristics of a airplane configuration including effects of canard and wing trailing-edge flap controls in combination /

Spencer, Bernard.
Sleeman, William C.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Supersedes NASA...

Aerodynamic characteristics of a 1/4-inch scale model a tilt-wing VTOL aircraft at high angles of wing incidence /

Tosti, Louis P.
United States. National Aeronautics and Space Administration.

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

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail /

Hieser, Gerald.
Reid, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 15, 1956."Includes bibliographical references (p. 17-18).Mode of access: Internet

Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title." June 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

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

Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ /

Trescot, Charles D.
Brooks, Cuyler W.
Putman, Lawrence E.
United States. National Aeronautics and Space Administration.

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

Aerodynamic characteristics of low-aspect-ratio wings in close proximity to the ground/

Fink, Marvin P.
Lastinger, James L.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and con...

Low-speed investigation of a full-span internal-flow jet-augmented flap on a high-wing model with a 35 degree swept wing of aspect ratio 7.0 /

Turner, Thomas R.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft, Aircraft; Stability and control.Includes bibliogra...

Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson.

Johnson, Joseph L.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogra...

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

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

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 canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond.

Spencer, Bernard.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Satellite...

Low-speed longitudinal characteristics of a airplane configuration including effects of canard and wing trailing-edge flap controls in combination /

Spencer, Bernard.
Sleeman, William C.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Supersedes NASA...

Aerodynamic characteristics of a 1/4-inch scale model a tilt-wing VTOL aircraft at high angles of wing incidence /

Tosti, Louis P.
United States. National Aeronautics and Space Administration.

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

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail /

Hieser, Gerald.
Reid, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 15, 1956."Includes bibliographical references (p. 17-18).Mode of access: Internet

Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title." June 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

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

Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ /

Trescot, Charles D.
Brooks, Cuyler W.
Putman, Lawrence E.
United States. National Aeronautics and Space Administration.

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

Aerodynamic characteristics of low-aspect-ratio wings in close proximity to the ground/

Fink, Marvin P.
Lastinger, James L.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and con...

Low-speed investigation of a full-span internal-flow jet-augmented flap on a high-wing model with a 35 degree swept wing of aspect ratio 7.0 /

Turner, Thomas R.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft, Aircraft; Stability and control.Includes bibliogra...

Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson.

Johnson, Joseph L.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogra...

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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

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