A Guide to the Use of the M.I.T. Cone Tables
- 1 May 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (5), 336-342
- https://doi.org/10.2514/8.3015
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Supersonic Flow over Conical Bodies Without Axial SymmetryJournal of the Aeronautical Sciences, 1953
- Supersonic Flow Around Cones at Large YawJournal of the Aeronautical Sciences, 1952
- Proper Use of the M.I.T. Tables for Supersonic Flow Past Inclined ConesJournal of the Aeronautical Sciences, 1951
- First- and Second-Order Theory of Supersonic Flow Past Bodies of RevolutionJournal of the Aeronautical Sciences, 1951
- On Supersonic Flow Past A Slightly Yawing ConeJournal of Mathematics and Physics, 1948
- A Theory for the Buckling of Thin ShellsJournal of the Aeronautical Sciences, 1942
- Buckling of a Column With Non-Linear Lateral SupportsJournal of the Aeronautical Sciences, 1942
- The Influence of Curvature on the Buckling Characteristics of StructuresJournal of the Aeronautical Sciences, 1940