The Rotational Field Behind a Curved Shock Wave Calculated by the Method of Flux Analysis
- 1 September 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (9), 830-845
- https://doi.org/10.2514/8.3670
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Calculation of Compressible Cascade Flow by the Method of Flux AnalysisJournal of the Aeronautical Sciences, 1954
- An Approximate Study on the Detached Shock Wave in front of a Circular Cylinder and a SphereJournal of the Physics Society Japan, 1953
- Über den abgelösten VerdichtungsstoßArchive of Applied Mechanics, 1951
- APPLICATION OF RELAXATION TO THE ROTATIONAL FIELD OF FLOW BEHIND A BOW SHOCK WAVEThe Quarterly Journal of Mechanics and Applied Mathematics, 1951
- On the Vorticity of the Flow Behind Curved ShockJournal of the Aeronautical Sciences, 1950
- A NOTE ON THE HODOGRAPH TRANSFORMATION FOR THE TWO-DIMENSIONAL VORTEX FLOW OF AN INCOMPRESSIBLE FLUIDThe Quarterly Journal of Mechanics and Applied Mathematics, 1950
- An Investigation of the Detached Shock in Front of a Body of RevolutionJournal of the Aeronautical Sciences, 1948
- On the Flow Behind Curved ShocksJournal of Mathematics and Physics, 1948
- Relaxation methods applied to engineering problems IX. High-speed flow of compressible fluid through a two-dimensional nozzlePhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1944
- Eine neue Stromfunktion für die Erforschung der Bewegung der Gase mit Rotation.ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1937