Aerodynamics of Rotary Wing and V/STOL Aircraft: Wind tunnel testing; new concepts in rotor control PDF Download
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Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 174
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Book Description
Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 174
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 792
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Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 100
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Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 186
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Author: Harry H. Heyson
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ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 340
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Book Description
Under sufficiently large wake deflections, the forward portion of the wake is found to flow forward along the floor leading to a vortex pattern which results in Rae's limits (Journal of Aircraft, May-June 1967). Although wind-tunnel data cannot normally be corrected successfully beyond these limits, it may be possible to obtain ground-effect data for conditions more severe than those implied by Rae.
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
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Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
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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 : Science
Languages : en
Pages : 256
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