Scientific and Technical Aerospace Reports
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Page : 938 pages
File Size : 32,74 MB
Release : 1987
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 938 pages
File Size : 32,74 MB
Release : 1987
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 580 pages
File Size : 12,90 MB
Release : 1956
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 818 pages
File Size : 46,38 MB
Release : 1954
Category : Aeronautics
ISBN :
Author : David J. Peake
Publisher :
Page : 64 pages
File Size : 17,85 MB
Release : 1982
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ISBN :
Author :
Publisher :
Page : 794 pages
File Size : 15,20 MB
Release : 1967
Category : Astronautics
ISBN :
Author : American Institute of Aeronautics and Astronautics
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 806 pages
File Size : 38,87 MB
Release : 1992
Category : Science
ISBN : 9781563470165
Prediction Methodology contains updated versions of nine chapters from the first edition and chapters on drag prediction, component build-up methods, Euler methods and Navier-Stokes solvers. Special attention is paid to nonlinear flow phenomena and unconventional airframe shapes. Eight colour plates and more than 540 figures are included.
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Page : 900 pages
File Size : 41,77 MB
Release : 1963
Category : Aeronautics
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Author :
Publisher :
Page : 400 pages
File Size : 50,6 MB
Release : 1948
Category : Mechanics, Applied
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Author : Royal Aeronautical Society
Publisher :
Page : 1110 pages
File Size : 14,87 MB
Release : 1959
Category : Aeronautics
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Author : G. J. Hancock
Publisher :
Page : 126 pages
File Size : 44,26 MB
Release : 1969
Category : Airplanes
ISBN :
Interpreting high angles of attack as those associated with stall and post-stall behaviour, the report reviews both aerodynamic and dynamic aspects. Dynamic considerations include stability and control response, and pre-stall and post-stall behaviour. Aerodynamic considerations range over a wide field covering two-dimensional stall characteristics, finite wing stall characteristics, including the effects of stall control devices, downwash at high angles, aircraft configuration force and moment characteristics, and aerodynamic derivative characteristics. Unsteady effects, Mach number effects, and propeller slipstream effects are included. (Author).