Wind-tunnel Testing of VTOL and STOL Aircraft PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Wind-tunnel Testing of VTOL and STOL Aircraft PDF full book. Access full book title Wind-tunnel Testing of VTOL and STOL Aircraft by . Download full books in PDF and EPUB format.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 86
Get Book
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 86
Get Book
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 78
Get Book
Book Description
Author: David H. Hickey
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24
Get Book
Book Description
The five aircraft tested represent a wide variety of V/STOL concepts. Correlation between the wind-tunnel and flight-test aerodynamic results is generally good when wind-tunnel wall corrections are omitted; in some cases wall corrections are shown to degrade the correlation. The aircraft and wind-tunnel geometry are related to model-tunnel sizing parameters and a VTOL lift parameter, in order to establish tentative sizing criteria for V/STOL wind-tunnel testing with small wall effects. The report is one of the series 515-522 of papers presented at the 27th meeting of the AGARD Flight Mechanics Panel, held 11-12 October 1965 in Rome, Italy. (Author).
Author: Lysle P. Parlett
Publisher:
ISBN:
Category : Jet transports
Languages : en
Pages : 90
Get Book
Book Description
Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with external flow jet flap.
Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 174
Get Book
Book Description
Author: Harry H. Heyson
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 340
Get Book
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: Alan Pope
Publisher: Wiley-Interscience
ISBN:
Category : Science
Languages : en
Pages : 562
Get Book
Book Description
Good,No Highlights,No Markup,all pages are intact, Slight Shelfwear,may have the corners slightly dented, may have slight color changes/slightly damaged spine.
Author: Marie H. Tuttle
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Get Book
Book Description
Author: Robert G. Mitchell
Publisher:
ISBN:
Category : Stalling (Aerodynamics)
Languages : en
Pages : 70
Get Book
Book Description
Author: David G. Koenig
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Get Book
Book Description