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Zhurnal Vychislitel'noi Matematiki i Matematicheskoi Fiziki, 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
Received: 07.03.1995 Revised: 27.06.1995
Citation:
V. V. Negoda, K. G. Sayadyan, “The use of transonic slender-body theory to calculate the spatial flow over a wing–fuselage configuration”, Zh. Vychisl. Mat. Mat. Fiz., 36:9 (1996), 134–154; Comput. Math. Math. Phys., 36:9 (1996), 1277–1293
Linking options:
https://www.mathnet.ru/eng/zvmmf9212 https://www.mathnet.ru/eng/zvmmf/v36/i9/p134
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Statistics & downloads: |
Abstract page: | 162 | Full-text PDF : | 99 | References: | 45 | First page: | 1 |
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