Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.19 chord below wing

Data from a static-thrust investigation of a large-scale general research vtol-stol model in ground effect /

Huston, Robert J.
Winston, Matthew M.

The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller di...

COMPARISON OF SEMISPAN AM) FULL-SPAN TESTS OF A 47.5 ' SW"m WING KITH SYMMEZRICAL CIRCuLAR4RC SECTIONS AND EAVING DROOPED-NOSE FLPSS,

Stanley Lipson
U. Reed Barnett
Stanley Lipson
U. Reed Barnett

January 1951

I In order t o help evaluate the general. va l id i ty of the semispan wing tes t ing technique in t...

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...

Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing

Fink, M. P.

January 1969

Aerodynamic characteristics of large semi-span V/STOL tilt-wing with single propeller tested for mod...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing

Kink, M. P.

July 1967

Longitudinal aerodynamic characteristics of large scale semispan V/STOL tilt-wing configuration havi...

Aerodynamic data on a large semispan tilting wing with a 0.5-diameter chord, a double-slotted flap, and left-hand and right-hand rotation of a single propeller, in presence of fuselage

Fink, M. P.

November 1966

Aerodynamic characteristics of large semispan tilting wing model having double-slotted flap, rotatin...

Pressure Distribution of a Large Semispan Tilting Wing with 0.4-diameter-chord, Single- Slotted Flap, and a Single Propeller 0.22 Chord Below Wing

Fink, M. P.
Smith, C. C., Jr.

October 1969

Aerodynamic pressure distribution on semispan tilting wing-propeller combination of V/STOL aircraf

Aerodynamic data on a large semispan tilting wing with a 0.5-diameter chord, a single slotted flap and both left-hand and right-hand rotation of a single propeller

Fink, M. P.
Mitchell, R. G.

February 1967

Longitudinal aerodynamic characteristics of large semispan V/STOL tilt-wing configuration with singl...

Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing /

Fink, Marvin P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N 69-17312.Cover title.Includes bibliographical references (p. 1...

Aerodynamic data on a large semispan tilting wing with 0.6-diameter chord, fowler flap, and single propeller rotating up at tip

White, L. C.
Mitchell, R. G.
Fink, M. P.

February 1964

Longitudinal aerodynamic characteristics of semispan v/stol tilt-wing configuration with single rota...

Aerodynamic data on a large semispan tilting wing with 0.5-diameter chord, double-slotted flap, and both left-hand and right-hand rotation of a single propeller

White, L. C.
Mitchell, R. G.
Fink, M. P.

April 1966

Longitudinal aerodynamic data on large-scale semispan V/STOL tilt-wing configuration having single p...

Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight /

Goodson, Kenneth W.
Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1962

"An investigation of the aerodynamic characteristics of a powered semispan tilting-shrouded-propelle...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing /

Fink, Marvin P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Large scale wind tunnel investigation of a semispan wing equipped with an externally-blown jet flap

Aiken, T. N.
Falarski, M. D.

July 1971

A wind tunnel investigation was made of the aerodynamic characteristics of a 14.5 foot semispan, ext...

Aerodynamic data on large semispan tilting wing with 0.6 -diameter chord, single slotted flap and single propeller rotating up at tip

Fink, Marvin P.
White, Lucy C.
Mitchell, Robert G.
United States. National Aeronautics and Space Administration.

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

Data from a static-thrust investigation of a large-scale general research vtol-stol model in ground effect /

Huston, Robert J.
Winston, Matthew M.

The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller di...

COMPARISON OF SEMISPAN AM) FULL-SPAN TESTS OF A 47.5 ' SW"m WING KITH SYMMEZRICAL CIRCuLAR4RC SECTIONS AND EAVING DROOPED-NOSE FLPSS,

Stanley Lipson
U. Reed Barnett
Stanley Lipson
U. Reed Barnett

January 1951

I In order t o help evaluate the general. va l id i ty of the semispan wing tes t ing technique in t...

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...

Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing

Fink, M. P.

January 1969

Aerodynamic characteristics of large semi-span V/STOL tilt-wing with single propeller tested for mod...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing

Kink, M. P.

July 1967

Longitudinal aerodynamic characteristics of large scale semispan V/STOL tilt-wing configuration havi...

Aerodynamic data on a large semispan tilting wing with a 0.5-diameter chord, a double-slotted flap, and left-hand and right-hand rotation of a single propeller, in presence of fuselage

Fink, M. P.

November 1966

Aerodynamic characteristics of large semispan tilting wing model having double-slotted flap, rotatin...

Pressure Distribution of a Large Semispan Tilting Wing with 0.4-diameter-chord, Single- Slotted Flap, and a Single Propeller 0.22 Chord Below Wing

Fink, M. P.
Smith, C. C., Jr.

October 1969

Aerodynamic pressure distribution on semispan tilting wing-propeller combination of V/STOL aircraf

Aerodynamic data on a large semispan tilting wing with a 0.5-diameter chord, a single slotted flap and both left-hand and right-hand rotation of a single propeller

Fink, M. P.
Mitchell, R. G.

February 1967

Longitudinal aerodynamic characteristics of large semispan V/STOL tilt-wing configuration with singl...

Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing /

Fink, Marvin P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N 69-17312.Cover title.Includes bibliographical references (p. 1...

Aerodynamic data on a large semispan tilting wing with 0.6-diameter chord, fowler flap, and single propeller rotating up at tip

White, L. C.
Mitchell, R. G.
Fink, M. P.

February 1964

Longitudinal aerodynamic characteristics of semispan v/stol tilt-wing configuration with single rota...

Aerodynamic data on a large semispan tilting wing with 0.5-diameter chord, double-slotted flap, and both left-hand and right-hand rotation of a single propeller

White, L. C.
Mitchell, R. G.
Fink, M. P.

April 1966

Longitudinal aerodynamic data on large-scale semispan V/STOL tilt-wing configuration having single p...

Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight /

Goodson, Kenneth W.
Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1962

"An investigation of the aerodynamic characteristics of a powered semispan tilting-shrouded-propelle...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing /

Fink, Marvin P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Large scale wind tunnel investigation of a semispan wing equipped with an externally-blown jet flap

Aiken, T. N.
Falarski, M. D.

July 1971

A wind tunnel investigation was made of the aerodynamic characteristics of a 14.5 foot semispan, ext...

Aerodynamic data on large semispan tilting wing with 0.6 -diameter chord, single slotted flap and single propeller rotating up at tip

Fink, Marvin P.
White, Lucy C.
Mitchell, Robert G.
United States. National Aeronautics and Space Administration.

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

Data from a static-thrust investigation of a large-scale general research vtol-stol model in ground effect /

Huston, Robert J.
Winston, Matthew M.

The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller di...

COMPARISON OF SEMISPAN AM) FULL-SPAN TESTS OF A 47.5 ' SW"m WING KITH SYMMEZRICAL CIRCuLAR4RC SECTIONS AND EAVING DROOPED-NOSE FLPSS,

Stanley Lipson
U. Reed Barnett
Stanley Lipson
U. Reed Barnett

January 1951

I In order t o help evaluate the general. va l id i ty of the semispan wing tes t ing technique in t...

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...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.19 chord below wing

Abstract

Extracted data

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.19 chord below wing

Abstract

Extracted data

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