Finite element analysis of conductive and radiative heating of a thin skin calorimeter

Author:

Mehta R. C.,Jayachandran T.,Sastri V. M. K.

Publisher

Springer Science and Business Media LLC

Subject

General Engineering

Reference10 articles.

1. Rumsey, C. B.; Lee, D. B.: Measurement of aerodynamic heat transfer on a l5° cone-cylinder-flare configuration in free flight at Mach numbers up to 4.7, NASA TND 824, 1961

2. Rumsey, C. B.; Lee, D. B.: Measurements of aerodynamic heat transfer and boundary-layer transition on a 15° cone in free flight at supersonic Mach number up to 5.2, NASA TND 888, 1961

3. Rumsey, C. B.; Lee, D. B.: Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9, NASA TND 745, 1961

4. Kidd, C. T.: Thin-skin technique heat-transfer measurement errors due to heat conduction into thermocouple wires. ISA Transaction. (1985) 1–10

5. Conti, R. J.: Approximate temperature distributions and streamwise heat conduction effects in the transient aerodynamic heating of thin-skinned bodies. NASA TND-895, 1961

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