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Effects of Subsonic, Supersonic, Hypersonic, and Orbital Environments on Structures
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English
Abstract
Preliminary selection of basic materials for flight vehicles is based on Mach number-altitude orientation, which includes turbulent flow to laminar flow location and effects. Structural weights and materials as a function of temperature are presented for both protected and unprotected primary structures. Design considerations and material selections for other pertinent items such as inlets, nose cones, leading edges, and transparencies are also considered.
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Citation
McBee, O., "Effects of Subsonic, Supersonic, Hypersonic, and Orbital Environments on Structures," SAE Technical Paper 660671, 1966, https://doi.org/10.4271/660671.Also In
References
- Pagel L. L. Beardsley P. P. Gaumer G. R. “Asset-Correlative Analysis of Heat Transfer Data,” AFFDL-TR-65-31 IV April 1966 35