Transient surface temperatures in rocket nozzles

descriptionPublicationkeyboard_double_arrow_right Article 01 Mar 1964 English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:Journal of Spacecraft and Rockets, volume 1, pages 219-221 (issn: 0022-4650, eissn: 1533-6794,

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Authors: GEORGE T. Y. CHAO; JOHN A. JACOBSEN; JAMES T. ANDERSON;

doi: 10.2514/3.27632

Transient surface temperatures in rocket nozzles

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Abstract

c = specific heat of solid, Btu/lb-°F d = half-thickness of node, in. erf = error function h = heat-transfer coefficient, convective plus radiant heating, Btu/sec-in.-°F = thermal conductivity of solid, Btu/sec-in.-°F/in. Mn = eigen values of MntsinMn = NBI NBI = Biot number, NBI = hd/k NFO = Fourier modulus, NFO = &0/8 n = number of eigenvalues T = temperature, °F a — thermal diffusivity, in./sec d = thickness of plate, in. 6 = time, sec p = density, Ib /in.

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