Aerodynamics of Rotary Wing and V/STOL Aircraft: Wind tunnel testing; new concepts in rotor control

Aerodynamics of Rotary Wing and V/STOL Aircraft: Wind tunnel testing; new concepts in rotor control PDF Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 174

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Aerodynamics of Rotary Wing and V/STOL Aircraft: Wind tunnel testing; new concepts in rotor control

Aerodynamics of Rotary Wing and V/STOL Aircraft: Wind tunnel testing; new concepts in rotor control PDF Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 174

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Cal/avlabs Symposium Proceedings (3rd), 18-20 June 1969, Buffalo, New York. Aerodynamics of Rotary Wing and V/stol Aircraft. Volume Ii. Wind Tunnel Testing. New Concepts in Rotor Control

Cal/avlabs Symposium Proceedings (3rd), 18-20 June 1969, Buffalo, New York. Aerodynamics of Rotary Wing and V/stol Aircraft. Volume Ii. Wind Tunnel Testing. New Concepts in Rotor Control PDF Author: CORNELL AERONAUTICAL LAB INC BUFFALO N Y.
Publisher:
ISBN:
Category :
Languages : en
Pages : 312

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Contents: Model vs. full scale rotor testing; The flow throughout a wind tunnel containing a rotor with a sharply deflected wake; Comments on V/STOL wind tunnel data at low forward speeds; Problems associated with tunnel tests of high disk loading systems at low forward speeds; Some research on rotor circulation control; The aerodynamics of a circulation-controlled rotor; Higher harmonic pitch control; and The controllable twist rotor.

Aerodynamics of Rotary Wing and V/STOL Aircraft: Featured speakers, panel session on recommendations for future aerodynamic research

Aerodynamics of Rotary Wing and V/STOL Aircraft: Featured speakers, panel session on recommendations for future aerodynamic research PDF Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 100

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Wind Tunnel Testing

Wind Tunnel Testing PDF Author: Cornell Aeronautical Laboratory
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Aerodynamics of Rotary Wing and V/STOL Aircraft

Aerodynamics of Rotary Wing and V/STOL Aircraft PDF Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 186

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 792

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64

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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 : 966

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Theoretical Study of Conditions Limiting V/STOL Testing in Wind Tunnels with Solid Floor

Theoretical Study of Conditions Limiting V/STOL Testing in Wind Tunnels with Solid Floor PDF Author: Harry H. Heyson
Publisher:
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.

NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing

NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing PDF 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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