The Effect of Heat Transfer on the Behavior of a Compressible Laminar Boundary Layer Under Favorable and Adverse Pressure Gradients

作者: Ting-Yi Li , H. T. Nagamatsu

DOI: 10.2514/8.3238

关键词: Pressure gradientLaminar flowCompressibilityMechanicsFlow separationBoundary layerHeat transferMaterials science

摘要:

参考文章(4)
Ting-Yi Li, Henry T. Nagamatsu, Similar Solutions of Compressible Boundary-Layer Equations Journal of the Aeronautical Sciences. ,vol. 20, pp. 653- 655 ,(1953) , 10.2514/8.2781
V.M. Falkneb, S.W. Skan, LXXXV. Solutions of the boundary-layer equations Philosophical Magazine Series 1. ,vol. 12, pp. 865- 896 ,(1931) , 10.1080/14786443109461870
D. R. Hartree, Bertha Swirles, The effect of configuration interaction on the low terms of the spectra of oxygen Mathematical Proceedings of the Cambridge Philosophical Society. ,vol. 33, pp. 240- 249 ,(1937) , 10.1017/S0305004100019587
C. R. ILLINGWORTH, THE EFFECT OF HEAT TRANSFER ON THE SEPARATION OF A COMPRESSIBLE LAMINAR BOUNDARY LAYER Quarterly Journal of Mechanics and Applied Mathematics. ,vol. 7, pp. 8- 34 ,(1954) , 10.1093/QJMAM/7.1.8