Introduction to V-STOL Airplanes PDF Download
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Author: David L. Kohlman
Publisher:
ISBN: 9780608001265
Category :
Languages : en
Pages : 243
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Book Description
Author: David L. Kohlman
Publisher:
ISBN: 9780608001265
Category :
Languages : en
Pages : 243
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Book Description
Author: Barnes Warnock McCormick
Publisher: Courier Corporation
ISBN: 9780486404608
Category : Technology & Engineering
Languages : en
Pages : 356
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Book Description
An extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.
Author: Michael J. Hirschberg
Publisher: AIAA
ISBN: 9781563472480
Category : History
Languages : en
Pages : 100
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Book Description
This important case study reports on the V/STOL development activities in the Soviet Union. As in the West, the Soviets also began using flying test rigs in the late 1950s. By combining the lift engines with modifications to existing engines, the Soviets were able to deploy the Yak-38 Forger only two years after the Harrier. The Forger was in service for 15 years before the political situation forced its retirement from service. Packed with illustrations, references, glossaries, and bibliographies, this case study is a necessary resource for the studies of V/STOL aircraft and systems designers.
Author: James A. Franklin
Publisher: AIAA
ISBN: 9781600860478
Category : Airplanes
Languages : en
Pages : 240
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Book Description
Annotation This text presents the principles of dynamics and control for vertical, short take-off landing (V/STOL) aircraft. It is the first book of its kind. It is intended for graduate students and professionals in aeronautics who have knowledge of linear systems analysis, aircraft static, dynamic stability, and control. The text begins with a discussion of V/STOL aircraft operations. Control strategies, equations of motion, longitudinal and lateral-directional flying qualities in both hover and forward flight, wind and turbulence responses, and control augmentation and cockpit displays are covered. Specific examples of the YAV-8B Harrier and XV-15 Tilt Rotor aircraft are used to illustrate actual V/STOL dynamic and control characteristics.
Author: Franklin D. Harris
Publisher:
ISBN:
Category : Autogiros
Languages : en
Pages :
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Book Description
Author:
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 8
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Book Description
Author: United States. Congress. House. Committee on Armed Services
Publisher:
ISBN:
Category : Legislative hearings
Languages : en
Pages : 600
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Book Description
Author:
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 486
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Book Description
Author: Seth B. Anderson
Publisher:
ISBN:
Category : Flight control
Languages : en
Pages : 56
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Book Description
A study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the current military requirements for helicopters and airplanes as a framework, modifications and additions were made for conversion to a preliminary set of V/STOL requirements using a broad background of flight experience and pilots' comments from VTOL and STOL aircraft, BLC (boundary-layer-control) equipped aircraft, variable stability aircraft, flight simulators and landing approach studies. The report contains a discussion of the reasoning behind and the sources of information leading to suggested requirements. The results of the study indicate that the majority of V/STOL requirements can be defined by modifications to the helicopter and/or airplane requirements by appropriate definition of reference speeds. Areas where a requirement is included but where the information is felt to be inadequate to establish a firm quantitative requirement include the following: Control power and damping relationships about all axes for various sizes and types of aircraft; control power, sensitivity, d-amping and response for height control; dynamic longitudinal and dynamic lateral- directional stability in the transition region, including emergency operation; hovering steadiness; acceleration and deceleration in transition; descent rates and flight-path angles in steep approaches, and thrust margin for approach.
Author:
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 616
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Book Description
