Simplified expressions for determining heat transfer to several aircraft shapes at hypersonic speeds are used to examine basis for choosing particular class of structure to withstand aerodynamic heating by either re-radiation, absorption through temperature rise of mass, or by phase change of structure; examples of ways to recover data capsule from satellite; re-entry vehicles containing capsule include lifting and non-lifting aircraft. (received Mar 1960)
Influence of aerodynamic heating on structural design of aircraft
AGARD -- Report
AGARD -- Reports ; n 207
1958
22 pages
Report
Englisch
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Aerodynamic heating of aircraft components
NTRS | 1955
|Aerodynamic heating of aircraft components
NTRS | 1956
|Aerodynamic heating of aircraft components
NTRS | 1956
|