12 November 1993 Infrared missile domes: heat flux and thermal shock
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Abstract
Analytical expressions for the thermal shock resistance (TSR) of IR missile domes involve a phenomenological stress factor that is not yet available but can be either extracted from the results of aerothermal shock testing or estimated on the basis of model-related considerations. The primary purpose of this contribution is to derive a simple formula for the allowable heat flux at the stagnation point, under conditions such that the boundary-layer flow remains laminar over the entire dome surface.
© (1993) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Claude A. Klein, "Infrared missile domes: heat flux and thermal shock", Proc. SPIE 1997, High Heat Flux Engineering II, (12 November 1993); doi: 10.1117/12.163797; https://doi.org/10.1117/12.163797
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