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 /

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

Capone, Francis J.
Arbiter, Dorothy.
Bare, E. Ann.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode...

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

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...

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...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

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...

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...

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

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

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

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...

Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /

Yancey, Roxanah B.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 /

Gillespie Jr., Warren.
Langley Research Center.

Prepared at the Langley Research Center, Langley Field, VA.Cover title."October 1960."--Cover.Includ...

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

Capone, Francis J.
Arbiter, Dorothy.
Bare, E. Ann.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode...

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

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...

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...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

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...

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...

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

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

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

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...

Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /

Yancey, Roxanah B.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 /

Gillespie Jr., Warren.
Langley Research Center.

Prepared at the Langley Research Center, Langley Field, VA.Cover title."October 1960."--Cover.Includ...

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

Capone, Francis J.
Arbiter, Dorothy.
Bare, E. Ann.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode...

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

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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

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