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similar law stress heat wing shown differenti equat heat plate larg temperatur gradient similar plate constant temperatur made proper modif thick load isotherm plate fact lead result stress heat plate calcul measur strain unheat plate seri relat call similar law applic analog theori solid wing aerodynam heat discuss detail load unheat analog wing howev complic involv novel concept feedback bodi forc load problem stress heat box wing structur solv analog method briefli discuss