Second-Order Methods in Inviscid Supersonic Theory
- 1 December 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (12) , 851-852
- https://doi.org/10.2514/8.3240
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- THE EFFECT OF HEAT TRANSFER ON THE SEPARATION OF A COMPRESSIBLE LAMINAR BOUNDARY LAYERThe Quarterly Journal of Mechanics and Applied Mathematics, 1954
- Similar Solutions of Compressible Boundary-Layer EquationsJournal of the Aeronautical Sciences, 1953
- First- and Second-Order Theory of Supersonic Flow Past Bodies of RevolutionJournal of the Aeronautical Sciences, 1951
- The effect of configuration interaction on the low terms of the spectra of oxygenMathematical Proceedings of the Cambridge Philosophical Society, 1937
- LXXXV.Solutions of the boundary-layer equationsJournal of Computers in Education, 1931