TY  - JOUR
AB  - IN very high performance aircraft—that is aircraft flying at high speeds and high altitudes—the thermal problems confronting the mechanical engineer are becoming progressively more and more severe. Atmospheric Temperature ranges of upwards of 100 deg. C combined with thermodynamic effects due to the high speeds, widely varying air pressure and moisture content are encountered and very rigid temperature limits for the various component parts of the aircraft have to be met with equipment of a minimum size and weight and without materially affecting the overall performance of the machine.
VL  - 26
IS  - 7
SN  - 0002-2667
DO  - 10.1108/eb032443
UR  - https://doi.org/10.1108/eb032443
AU  - Rendel David
PY  - 1954
Y1  - 1954/01/01
TI  - Thermal Problems of High Performance Flight: A Further Contribution to the Bristol Conference on Thermal Stress Organized by the Stress Analysis Group of the Institute of Physics
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 220
EP  - 223
Y2  - 2024/04/19
ER  -