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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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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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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NASA Technical Note

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

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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 : 44

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An Analytical Study of V/STOL Handling Qualities in Hover and Transition

An Analytical Study of V/STOL Handling Qualities in Hover and Transition PDF Author: R. L. Stapleford
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ISBN:
Category : Airplanes
Languages : en
Pages : 174

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The hover analysis considers pilot attitude and position control tasks in the presence of horizontal gusts. The effects of each of the stability derivatives on the difficulty of the control tasks and on the closed-loop gust responses are determined. It is clearly shown that the handling qualities studies of control sensitivity and angular damping must consider the influences of M sub u (or L sub v) and should include gust inputs. These conclusions are substantiated by previous variable-stability-helicopter experiments. The effects of vehicle size and geometry are investigated by several approaches. The key result of increasing size is found to be a reduction in M sub u and L sub v which can, in turn, lower the requirements for control power and damping. The handling qualities during transition of two vehicles, a tilt duct and a tilt wing, which were previously tested on a simulator are analyzed. It is shown that both trim control and perturbations about the trim conditions must be considered. In fact, part of the increased difficulty in landing transitions, in comparison with takeoff transitions, is due to more difficult trim control; the much more stringent position control requirements in landing are also a contributing factor.

Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap

Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap PDF Author: Jerry V. Kirk
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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ISBN:
Category : Aeronautics
Languages : en
Pages : 260

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450

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U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 516

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Keywords Index to U.S. Government Technical Reports

Keywords Index to U.S. Government Technical Reports PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160

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