Zobrazeno 1 - 10
of 170
pro vyhledávání: '"W. F. Hilton"'
Autor:
Malkin, M. S.
Publikováno v:
American Scientist, 1977 Jan 01. 65(1), 91-92.
Externí odkaz:
https://www.jstor.org/stable/27847648
Publikováno v:
The Military Engineer, 1951 Sep 01. 43(295), 388-388.
Externí odkaz:
https://www.jstor.org/stable/44561421
Autor:
John E. Allen
Publikováno v:
Journal of the Royal Aeronautical Society. 70:678-679
Autor:
J. L. Nayler
Publikováno v:
The Aeronautical Journal. 76:63-63
Autor:
W. F. Hilton
Publikováno v:
The Aeronautical Journal. 95:71-71
Autor:
W. F. Hilton
Publikováno v:
The Aeronautical Journal. 94:265-265
Autor:
W. F. Hilton
Publikováno v:
The Aeronautical Journal. 94:75-75
Publikováno v:
Wind Energy; Oct2024, Vol. 27 Issue 10, p994-1010, 17p
Autor:
W. F. Hilton
Publikováno v:
The Journal of the Royal Aeronautical Society. 55:751-761
A start is made by considering why the subsonic propeller was abandoned when aircraft speeds approached the shock stall. It is true that the shock stall also occurs on the propeller blades under these conditions, causing a loss of lift and an increas
Autor:
W. F. Hilton
Publikováno v:
The Journal of the Royal Aeronautical Society. 55:43-51
Measurements were made of the downwash effects behind two finite wings 3.1 percent, thick, having square and 20° raked tips respectively. The tests were conducted at a Mach number of 1.45 and a Reynolds number of 1.2 millions by traversing a yawmete