Hypersonic flows over slender circular cones at small angles of attack
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Publication:3989883
DOI10.1016/0094-5765(91)90053-8zbMath0739.76027OpenAlexW1975321398MaRDI QIDQ3989883
Publication date: 28 June 1992
Published in: Acta Astronautica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/0094-5765(91)90053-8
perturbation theoryshock wavehypersonic flowsNewtonian flowsurface pressuresmall angles of attackdelta wingspointed-nose slender bodies
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