Large-Scale Wind-Tunnel Tests of a Wingless Vertical Take-Off and Landing Aircraft: Preliminary Results PDF Download

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Large-Scale Wind-Tunnel Tests of a Wingless Vertical Take-Off and Landing Aircraft: Preliminary Results

Large-Scale Wind-Tunnel Tests of a Wingless Vertical Take-Off and Landing Aircraft: Preliminary Results PDF Author: David G. Koenig
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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Book Description

Large-Scale Wind-Tunnel Tests of a Wingless Vertical Take-Off and Landing Aircraft: Preliminary Results

Large-Scale Wind-Tunnel Tests of a Wingless Vertical Take-Off and Landing Aircraft: Preliminary Results PDF Author: David G. Koenig
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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Book Description

A Large-scale Wind-tunnel Investigation of a Wingless Vertical Take-off and Landing Aircraft

A Large-scale Wind-tunnel Investigation of a Wingless Vertical Take-off and Landing Aircraft PDF Author: David G. Koenig
Publisher:
ISBN:
Category :
Languages : en
Pages : 56

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Book Description

A Large-scale Wind-tunnel Investigation of a Wingless Vertical Take-off and Landing Aircraft

A Large-scale Wind-tunnel Investigation of a Wingless Vertical Take-off and Landing Aircraft PDF Author: David G. Koenig
Publisher:
ISBN:
Category :
Languages : en
Pages : 48

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Book Description

Full-scale Wind-tunnel Tests of a Low-aspect-ratio, Straight-wing Airplane with Blowing Boundary-layer Control on Leading- and Trailing-edge Flaps

Full-scale Wind-tunnel Tests of a Low-aspect-ratio, Straight-wing Airplane with Blowing Boundary-layer Control on Leading- and Trailing-edge Flaps PDF Author: Mark W. Kelly
Publisher:
ISBN:
Category : Trailing edge flaps
Languages : en
Pages : 32

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Book Description

Large-scale Wind-tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust

Large-scale Wind-tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust PDF Author: Wallace H. Deckert
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 46

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Book Description
Tests were conducted to determine the wing stall, performance, and longitudinal stability and control characteristics of a large model of a V/STOL tilt-wing transport aircraft. The scope of the tests was limited primarily to the low-speed transitional regime.

Wind Tunnel Tests of a 0.65 Scale Ejection Seat with and Without Yaw Stabilizers

Wind Tunnel Tests of a 0.65 Scale Ejection Seat with and Without Yaw Stabilizers PDF Author: Peter Ayoub
Publisher:
ISBN:
Category : Pilot ejection seats
Languages : en
Pages : 224

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Book Description

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps PDF Author: James A. Weiberg
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38

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Book Description

Wind Tunnel Tests of Fuselages and Windscreens

Wind Tunnel Tests of Fuselages and Windscreens PDF Author: Edward Pearson Warner
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 552

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Book Description
The tests described herein were made in 1918, in the old four-foot wind tunnel at the Massachusetts Institute of Technology and at the request of the Engineering Division of the U.S. Army Air Service.

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 788

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Book Description

Theoretical Study of Conditions Limiting V/STOL Testing in Wind Tunnels with Solid Floor

Theoretical Study of Conditions Limiting V/STOL Testing in Wind Tunnels with Solid Floor PDF Author: Harry H. Heyson
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 340

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Book Description
Under sufficiently large wake deflections, the forward portion of the wake is found to flow forward along the floor leading to a vortex pattern which results in Rae's limits (Journal of Aircraft, May-June 1967). Although wind-tunnel data cannot normally be corrected successfully beyond these limits, it may be possible to obtain ground-effect data for conditions more severe than those implied by Rae.