Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 174
Book Description
Aerodynamics of Rotary Wing and V/STOL Aircraft: Wind tunnel testing; new concepts in rotor control
Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 174
Book Description
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 174
Book Description
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
Author: CORNELL AERONAUTICAL LAB INC BUFFALO N Y.
Publisher:
ISBN:
Category :
Languages : en
Pages : 312
Book Description
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.
Publisher:
ISBN:
Category :
Languages : en
Pages : 312
Book Description
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
Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 100
Book Description
Wind Tunnel Testing
Author: Cornell Aeronautical Laboratory
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Aerodynamics of Rotary Wing and V/STOL Aircraft
Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 186
Book Description
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 186
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 792
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 792
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
Theoretical Study of Conditions Limiting V/STOL Testing in Wind Tunnels with Solid Floor
Author: Harry H. Heyson
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 340
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.
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 340
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
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
Book Description