Thermal Stresses and Deflections in Rectangular Panels. Part II - The Analysis of Rectangular Panels with Three-Dimensional Heat Inputs
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Report Number: ASD TR 61-537 Part 2
Author(s): Newman, M., Forray, M. J.
Corporate Author(s): Republic Aviation Corporation
Date of Publication: 1962-10
Pages: 48
DoD Task:
Identifier: AD0293830
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Newman, M., Forray, M. J.
Corporate Author(s): Republic Aviation Corporation
Date of Publication: 1962-10
Pages: 48
DoD Task:
Identifier: AD0293830
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control