Author : William H. Dorrance
Publisher :
Page : 14 pages
File Size : 19,75 MB
Release : 1949
Category : Aerodynamics, Supersonic
ISBN :
Author :
Publisher :
Page : 776 pages
File Size : 18,77 MB
Release : 1971
Category : Mechanics, Applied
ISBN :
Author : D. Adamson
Publisher :
Page : 366 pages
File Size : 13,95 MB
Release : 1961
Category : Aerodynamics, Supersonic
ISBN :
Author : Franklin Moore
Publisher :
Page : 756 pages
File Size : 34,20 MB
Release : 1950
Category : Aerodynamics, Supersonic
ISBN :
First-order relations were obtained for attenuation of shock and flow deflection outward along the shock. These relations probably conform closely to physical fact, provided the entrance slope is small. These relations contain an error, but become exact as the radial coordinate approaches inifinity. The error is thus probably of the second order over the entire shock front.
Author : Johns Hopkins University. Applied Physics Laboratory
Publisher :
Page : 372 pages
File Size : 37,32 MB
Release : 1961
Category : Aerodynamics, Supersonic
ISBN :
Author : Leland H. Jorgensen
Publisher :
Page : 70 pages
File Size : 27,69 MB
Release : 1958
Category : Aerodynamics, Supersonic
ISBN :
Author :
Publisher :
Page : 646 pages
File Size : 26,15 MB
Release : 1983
Category : Aeronautics
ISBN :
Author : Roger H. Fournier
Publisher :
Page : 66 pages
File Size : 17,24 MB
Release : 1966
Category : Aerodynamics, Hypersonic
ISBN :
Author :
Publisher :
Page : 1610 pages
File Size : 46,36 MB
Release : 1948
Category : Engineering
ISBN :
Author : N. F. Krasnov
Publisher :
Page : 320 pages
File Size : 29,78 MB
Release : 1964
Category :
ISBN :
Topics include: pressure coefficient on a thin cone at very high Mach numbers; approximation of magnitude of pressure coefficient on the surface of a solid of revolution with arbitrary generatrix; approximation of magnitude of wave-drag coefficient; approximate evaluation of magnitude of lift coefficient; approximation of magnitude of moment coefficient and coefficient of center of pressure.
