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Application of the volterra method to calculation of interference between bodies of revolution and wings in supersonic flow

✍ Scribed by V. N. Mikhailov

Publisher
Springer
Year
1972
Tongue
English
Weight
222 KB
Volume
4
Category
Article
ISSN
0015-4628

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Application of a pseudo-viscous method to the calculation of the steady supersonic flow past a waisted body
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## Abstract A finite difference method for solving mixed initial and boundary value problems governed by hyperbolic partial differential equations is described. The method has been developed specifically to calculate the flow field associated with any arbitrary two‐dimensional or axi‐symmetric body