Linearized supersonic aerofoil theory part II
1947 ◽
Vol 240
(820)
◽
pp. 356-373
The operational approach to linearized supersonic aerofoil problems is further developed. In particular, the method is extended to give a general treatment of the drag on swept-back wings at zero incidence. Problems involving the lift on swept-back wings are also considered, and a recurrence method developed for obtaining the lift on a trapezoidal wing with tips swept back beyond the Mach angle. As a particular case this latter method is applied to the arrow-head wing.
1983 ◽
Vol 22
(02)
◽
pp. 77-82
◽
Keyword(s):
1978 ◽
Vol 43
(7)
◽
pp. 1907-1916
◽
Keyword(s):
Keyword(s):
1971 ◽
Vol 61
(6)
◽
pp. 773
◽
Keyword(s):
2007 ◽
Vol 22
(6)
◽
pp. 258-263
◽