Temperatures in plates subjected to a sudden increase in recovery temperature.
Abstract:ESDU 89026 treats the transient situation of the variation of the temperature distribution in a thick plate insulated on one side when the aerodynamic heating temperature on the other side suffers a step change from an initial constant temperature condition. Curves are given that allow the temperatures at both the heated and the insulated surfaces to be obtained at any time, and also to obtain an approximate value for the temperature at any point through the thickness of the plate from a knowledge of those surface values. A fully worked example illustrates the use of the method.
|Data Item ESDU 89026|
- Aircraft Noise
- Fatigue - Endurance Data
- Fatigue - Fracture Mechanics
- Fluid Mechanics, Internal Flow
- Fluid Mechanics, Internal Flow (Aerospace)
- Heat Transfer
- Physical Data, Chemical Engineering
- Stress and Strength
- Transonic Aerodynamics
- Vibration and Acoustic Fatigue
- Wind Engineering
Aerospace Materials Data
Additional Engineering References