Theoretical and Experimental Investigation of Thermal Stresses in Hypersonic-Aircraft Wing Structures
- 1 June 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (6) , 719-725
- https://doi.org/10.2514/8.9590
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Optimum Thin-Wall Pressure Vessels of Anisotropic MaterialsJournal of Applied Mechanics, 1966
- Correlation of Theoretical and Photothermoelastic Results on Thermal Stresses in Idealized Wing StructuresJournal of Applied Mechanics, 1960
- Physical Properties of Plastics for Photothermoelastic InvestigationsJournal of Applied Mechanics, 1958
- A Simple Model Study of Transient Temperature and Thermal Stress Distribution Due to Aerodynamic HeatingJournal of the Aeronautical Sciences, 1957
- THE TRANSVERSE POTENTIAL FLOW PAST A BODY OF REVOLUTIONThe Quarterly Journal of Mechanics and Applied Mathematics, 1956
- Zur Berechnung der Potentialströmung um quergestellte LuftschiffkörperArchive of Applied Mechanics, 1931
- Foundations of Potential TheoryPublished by Springer Nature ,1929