Effects of ground proximity on the longitudinal aerodynamic characteristics of an unswept aspect-ratio-10 wing /

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

Longitudinal aerodynamic characteristics in ground effect of a large-scale, V/STOL model with four tilting ducted fans arranged in a dual tandem configuration /

Giullianetti, Demo J.
Maki, Ralph L.
Biggers, James C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Prepared at Ames Research Center."N67-39980."Includes bibliographical references (p. 6).Mode of acce...

Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing

Mineck, R. E.
Carter, A. W.

July 1974

An investigation has been conducted to determine the effect of ground proximity on the aerodynamic c...

Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing /

Mineck, Raymond E.
Carter, Arthur W.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Effect of ground proximity on the aerodynamic characteristics of aspect-ratio-1 airfoils with and without end plates /

Carter, Arthur W.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1961

An investigation has been made to determine the effect of ground proximity on the aerodynamic charac...

An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability below the Mach Number of Lift Divergence /

Axelson, John A.
Crown, J. Conrad, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.

An analysis is presented of the influence of wing aspect ratio and tail location on the effects of c...

Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration /

Coe, Paul L.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references.Mode of access: Internet

Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds /

Gloss, Blair B.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

A study of the aerodynamic characteristics of a propeller and wing including the effect of ground proximity

Harris, A.P

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:DX182209 / BLDSC - British Library D...

Aerodynamic interference effects caused by parallel-staged simple aerodynamic configurations at Mach numbers of 3 and 6 /

Decker, John P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...

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...

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

Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches

Pienaar, D van V

January 2000

Summary in English.The investigation of the stability of longitudinal motion of fixed wing aircraft ...

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

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

Longitudinal aerodynamic characteristics in ground effect of a large-scale, V/STOL model with four tilting ducted fans arranged in a dual tandem configuration /

Giullianetti, Demo J.
Maki, Ralph L.
Biggers, James C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Prepared at Ames Research Center."N67-39980."Includes bibliographical references (p. 6).Mode of acce...

Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing

Mineck, R. E.
Carter, A. W.

July 1974

An investigation has been conducted to determine the effect of ground proximity on the aerodynamic c...

Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing /

Mineck, Raymond E.
Carter, Arthur W.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Effect of ground proximity on the aerodynamic characteristics of aspect-ratio-1 airfoils with and without end plates /

Carter, Arthur W.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1961

An investigation has been made to determine the effect of ground proximity on the aerodynamic charac...

An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability below the Mach Number of Lift Divergence /

Axelson, John A.
Crown, J. Conrad, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.

An analysis is presented of the influence of wing aspect ratio and tail location on the effects of c...

Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration /

Coe, Paul L.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references.Mode of access: Internet

Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds /

Gloss, Blair B.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

A study of the aerodynamic characteristics of a propeller and wing including the effect of ground proximity

Harris, A.P

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:DX182209 / BLDSC - British Library D...

Aerodynamic interference effects caused by parallel-staged simple aerodynamic configurations at Mach numbers of 3 and 6 /

Decker, John P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...

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...

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

Longitudinal stability and control analysis and parameter sensitivity investigation of fixed wing aircraft in ground proximity using various aerodynamic approaches

Pienaar, D van V

January 2000

Summary in English.The investigation of the stability of longitudinal motion of fixed wing aircraft ...

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

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

Longitudinal aerodynamic characteristics in ground effect of a large-scale, V/STOL model with four tilting ducted fans arranged in a dual tandem configuration /

Giullianetti, Demo J.
Maki, Ralph L.
Biggers, James C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Prepared at Ames Research Center."N67-39980."Includes bibliographical references (p. 6).Mode of acce...

Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing

Mineck, R. E.
Carter, A. W.

July 1974

An investigation has been conducted to determine the effect of ground proximity on the aerodynamic c...

Effects of ground proximity on the longitudinal aerodynamic characteristics of an unswept aspect-ratio-10 wing /

Abstract

Extracted data

Effects of ground proximity on the longitudinal aerodynamic characteristics of an unswept aspect-ratio-10 wing /

Abstract

Extracted data

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