A Flight Examination of Operating Problems of V/STOL Aircraft in STOL Type Landing and Approach PDF Download
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Author: Robert C. Innis
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
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Book Description
Author: Robert C. Innis
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
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Book Description
Author: Robert C. Innis
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
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Book Description
Author: ROBERT C. INNIS
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
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Book Description
The operating envelope of a large twin-engined STOL aircraft has been examined and general limitations have been pointed out which the pilot must consider when choosing a minimum landing approach speed for STOL aircraft. The significance of satisfactory stability and control characteristics in this regard is discussed. The problems reviewed in the report would also be representative of those of a large, over-loaded VTOL aircraft operating in an STOL manner. (Author).
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 422
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Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 340
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Author: Seth B. Anderson
Publisher:
ISBN:
Category : Flight control
Languages : en
Pages : 58
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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: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 522
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1284
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Author: United States. Naval Air Systems Command
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 152
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