Transition Characteristics of a VTOL Aircraft Powered by Four Ducted Tandem Propellers PDF Download

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Transition Characteristics of a VTOL Aircraft Powered by Four Ducted Tandem Propellers

Transition Characteristics of a VTOL Aircraft Powered by Four Ducted Tandem Propellers PDF Author: Edwin E. Davenport
Publisher:
ISBN:
Category : Ducted fans
Languages : en
Pages : 64

Book Description


Transition Characteristics of a VTOL Aircraft Powered by Four Ducted Tandem Propellers

Transition Characteristics of a VTOL Aircraft Powered by Four Ducted Tandem Propellers PDF Author: Edwin E. Davenport
Publisher:
ISBN:
Category : Ducted fans
Languages : en
Pages : 64

Book Description


Aerodynamic Characteristics of Four-duct Tandem VTOL-aircraft Configurations

Aerodynamic Characteristics of Four-duct Tandem VTOL-aircraft Configurations PDF Author: William A. Newsom
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 160

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 480

Book Description


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
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 174

Book Description
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.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1492

Book Description


V/STOL Concepts in the United States: Past, Present, and Future

V/STOL Concepts in the United States: Past, Present, and Future PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52

Book Description


Index Aeronauticus

Index Aeronauticus PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 976

Book Description


VTOL/STOL Aircraft

VTOL/STOL Aircraft PDF Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 344

Book Description


NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1152

Book Description


NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1156

Book Description