On the PLK Method and the Supersonic Blunt-Body Problem
- 1 February 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (2) , 185-206
- https://doi.org/10.2514/8.9363
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- An Approximate Solution of the Direct Supersonic Blunt-Body Problem for Arbitrary Axisymmetric ShapesJournal of the Aerospace Sciences, 1960
- A CONTRIBUTION TO THE SOLUTION OF MIXED PROBLEMS OF TRANSONIC AERODYNAMICSPublished by Elsevier ,1959
- A REVIEW OF SOME RECENT DEVELOPMENTS IN HYPERSONIC FLOW**This work was supported by the United States Air Force through the Office of Scientific Research, Air Research and Development Command, under Contract AF 49 (638)-217, and through the Aeronautical Research Laboratory of Wright Air Development Center, under Contract No. 33 (616)-3265.Published by Elsevier ,1959
- Theoretical Investigation of the Flow Field About Blunt-Nosed Bodies in Supersonic FlightJournal of the Aerospace Sciences, 1958
- Stiffness and Deflection Analysis of Complex StructuresJournal of the Aeronautical Sciences, 1956
- The Poincaré-Lighthill-Kuo MethodPublished by Elsevier ,1956
- G. The Method of CharacteristicsPublished by Walter de Gruyter GmbH ,1954