Thermo-elastic equations for a sandwich panel under arbitrary temperature distribution, transverse load and edge compression /
Ibrahim K. Ebcioglu.

APA Citation

Ebcioglu, I. K.., United States. Air Force. Systems Command. Aeronautical Systems Division., United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States. (1961). Thermo-elastic equations for a sandwich panel under arbitrary temperature distribution, transverse load and edge compression. Wright-Patterson Air Force Base, Ohio: Aeronautical Systems Division, Air Force Systems Command, United States Air Force.

MLA Citation

Ebcioglu, Ibrahim K., United States. Air Force. Systems Command. Aeronautical Systems Division, and United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States. Thermo-elastic Equations for a Sandwich Panel Under Arbitrary Temperature Distribution, Transverse Load And Edge Compression. Wright-Patterson Air Force Base, Ohio: Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961.

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