Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
Assessment of Aerodynamic Performance of V/STOL and STOVL Fighter Aircraft
Author: Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
A Flight Examination of Operating Problems of V/STOL Aircraft in STOL Type Landing and Approach
Author: Robert C. InnisPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
Book Description
Powered-lift Aircraft Technology
Author: Wallace H. DeckertPublisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 44
Book Description
Review of Basic Principles of V/STOL Aerodynamics
Author: Richard E. KuhnPublisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
V/STOL Concepts in the United States: Past, Present, and Future
Author: The Aerodynamics of V/STOL Aircraft
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and DevelopmentPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 522
Book Description
Special Course on Subsonic/transonic Aerodynamic Interference for Aicraft
Author: Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 1204
Book Description
An Examination of Handling Qualities Criteria for V/STOL Aircraft
Author: Seth B. AndersonPublisher:
ISBN:
Category : Flight control
Languages : en
Pages : 58
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.
Special Course on V/STOL Aerodynamics
Author: Publisher:
ISBN: 9789283514893
Category : Aerodynamics
Languages : en
Pages : 18
Book Description
