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

Large-scale wind-tunnel tests of descent performance of an airplane model with a tilt wing and differential propeller thrust

Deckert, W. H.
Dickinson, S. O.
Page, V. R.

October 1964

Wind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/...

Investigation of Full-Scale Split Trailing-Edge Wing Flaps with Various Chords and Hinge Locations

Wallace, Rudolf

January 1936

This report gives the results of an investigation conducted in the NACA full-scale wind tunnel on a ...

Aerodynamic Characteristics of a Four-Propeller Tilt-Wing VTOL Model with Twin Vertical Tails, Including Effects of Ground Proximity

Grunwald, Kalman J.

June 1961

Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...

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

Fink, M. P.

April 1967

Wind tunnel tests to determine longitudinal aerodynamic characteristics of large scale semispan V/ST...

Exploratory investigation of the effectiveness of biplane wings with large-chord double slotted flaps in redirecting a propeller slipstream downward for vertical take-off

Kirby, Robert H

Results are presented from static-force tests on biplane wings with large-chord double slotted flaps...

Aerodynamic characteristics of a propeller-powered high-lift semispan wing

Applin, Zachary T.
Takallu, M. A.
Gentry, Garl L., Jr.

April 1994

A small-scale semispan high-lift wing-flap system equipped under the wing with a turboprop engine as...

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...

Large-Scale Wind-Tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing Flaps

Holzhauser, Curt A.
Weiberg, James A.

June 1961

Tests were made of a large-scale tilt-wing deflected-slipstream VTOL airplane with blowing-type BLC ...

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...

Wind tunnel investigation of a large-scale semispan model with an unswept wing and an upper-surface blown jet flat

Phelps, A. E., III
Smith, C. C., Jr.
Copeland, W. L.

February 1974

An investigation of the static longitudinal aerodynamic characteristics of a large-scale semispan mo...

Large-scale wind-tunnel tests of descent performance of an airplane model with a tilt wing and differential propeller thrust

Deckert, W. H.
Dickinson, S. O.
Page, V. R.

October 1964

Wind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/...

Investigation of Full-Scale Split Trailing-Edge Wing Flaps with Various Chords and Hinge Locations

Wallace, Rudolf

January 1936

This report gives the results of an investigation conducted in the NACA full-scale wind tunnel on a ...

Aerodynamic Characteristics of a Four-Propeller Tilt-Wing VTOL Model with Twin Vertical Tails, Including Effects of Ground Proximity

Grunwald, Kalman J.

June 1961

Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...

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

Fink, M. P.

April 1967

Wind tunnel tests to determine longitudinal aerodynamic characteristics of large scale semispan V/ST...

Exploratory investigation of the effectiveness of biplane wings with large-chord double slotted flaps in redirecting a propeller slipstream downward for vertical take-off

Kirby, Robert H

Results are presented from static-force tests on biplane wings with large-chord double slotted flaps...

Aerodynamic characteristics of a propeller-powered high-lift semispan wing

Applin, Zachary T.
Takallu, M. A.
Gentry, Garl L., Jr.

April 1994

A small-scale semispan high-lift wing-flap system equipped under the wing with a turboprop engine as...

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...

Large-Scale Wind-Tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing Flaps

Holzhauser, Curt A.
Weiberg, James A.

June 1961

Tests were made of a large-scale tilt-wing deflected-slipstream VTOL airplane with blowing-type BLC ...

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...

Wind tunnel investigation of a large-scale semispan model with an unswept wing and an upper-surface blown jet flat

Phelps, A. E., III
Smith, C. C., Jr.
Copeland, W. L.

February 1974

An investigation of the static longitudinal aerodynamic characteristics of a large-scale semispan mo...

Large-scale wind-tunnel tests of descent performance of an airplane model with a tilt wing and differential propeller thrust

Deckert, W. H.
Dickinson, S. O.
Page, V. R.

October 1964

Wind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/...

Investigation of Full-Scale Split Trailing-Edge Wing Flaps with Various Chords and Hinge Locations

Wallace, Rudolf

January 1936

This report gives the results of an investigation conducted in the NACA full-scale wind tunnel on a ...

Aerodynamic Characteristics of a Four-Propeller Tilt-Wing VTOL Model with Twin Vertical Tails, Including Effects of Ground Proximity

Grunwald, Kalman J.

June 1961

Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...

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

Abstract

Extracted data

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

Abstract

Extracted data

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