A First-Order Formulation of the Unsteady Supersonic Flow Problem for Finite Wings
- 1 June 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (6) , 578-582
- https://doi.org/10.2514/8.3611
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- The Delta Wing in a Non-Uniform Supersonic StreamAeronautical Quarterly, 1954
- On the transformation of the linearized equation of unsteady supersonic flowQuarterly of Applied Mathematics, 1954
- Increasing the Range of Axial-Flow Compressors by Use of Adjustable Stator BladesJournal of the Aeronautical Sciences, 1947
- Supersonic Wave Drag of Thin AirfoilsJournal of the Aeronautical Sciences, 1946