On Bodies Achieving Extreme Values of the Critical Mach Number, I-Reference-Cited by-同舟云学术

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On Bodies Achieving Extreme Values of the Critical Mach Number, I

Published:1954 Issue:2 Volume:3 Page:209-230
ISSN:0022-2518
Container-title:Indiana University Mathematics Journal
language:en
Short-container-title:Indiana Univ. Math. J.

Author:

Gilbarg D.,Shiffman M.

Publisher

Indiana University Mathematics Journal

Subject

General Mathematics

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Lift Airfoils Close to the Airfoils in a Flow with the Maximum “Critical” Mach Numbers;Известия Российской академии наук. Механика жидкости и газа;2023-01-01

2. О месте звуковых точек в критическом течении;Вестник Самарского государственного технического университета. Серия «Физико-математические науки»;2021

3. Compressible Subsonic Impinging Flows;Archive for Rational Mechanics and Analysis;2018-05-15

4. Variational method of constructing subsonic airfoil profiles;Journal of Applied Mechanics and Technical Physics;1992

5. Flow around axisymmetric bodies with three constant-velocity sections;Journal of Applied Mechanics and Technical Physics;1984

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