Zh. Vychisl. Mat. Mat. Fiz., 1996 Volume 36, Number 9, Pages 134–154
(Mi zvmmf9212)
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The use of transonic slender-body theory to calculate the spatial flow over a wing–fuselage configuration
V. V. Negoda,
K. G. Sayadyan Moscow
UDC:
519.6:533.7
Received: 07.03.1995
Revised: 27.06.1995
English version:
Computational Mathematics and Mathematical Physics, 1996,
36:9,
1277–1293
Bibliographic databases:
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