火箭发动机 (Chinese Wikipedia)

Analysis of information sources in references of the Wikipedia article "火箭发动机" in Chinese language version.

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aero.org

声振荡可由热过程激活，如管道中的热空气流，室内的燃烧。如果在室内声波压力最大处激烈燃烧，该处的驻声波会增长。根据Lord Rayleigh对热声学过程的准则，“如果给最大程度浓缩的空气加热，或在其最稀薄时撤走热量，振动被激发；反之，震荡被消弱”（参考： John Wm. Strutt, Baron Rayleigh, The Theory of Sound, 2nd ed. (London: Macmillan, 1896) (reprinted by Dover Publications (N.Y., N.Y.) in 1945), vol. 2, page 226.) 参见： (1) Lord Rayleigh (1878) "The explanation of certain acoustical phenomena" (namely, the Rijke tube) Nature, vol. 18, pages 319–321; and (2) E. C. Fernandes and M. V. Heitor, “Unsteady flames and the Rayleigh criterion” in F. Culick, M. V. Heitor, and J. H. Whitelaw, ed.s, Unsteady Combustion (Dordrecht, the Netherlands: Kluwer Academic Publishers, 1996), page 4. Available on-line at: http://books.google.com/books?id=Je_hG6UfnogC&pg=PA1&lpg=PA1&dq=%22rayleigh+criterion%22+%22unsteady+combustion%22&source=web&ots=nXDy37Yyjo&sig=1EiFKayOxSSJL9NhR6mlKQBRjf8&hl=en&sa=X&oi=book_result&resnum=4&ct=result#PPA4,M1

Huzel, D. K. and Huang, D. H. NASA SP-125, Design of Liquid Propellant Rocket Engines 2nd Edition. NASA. 1971 [2008-08-12]. （原始内容存档于2020-12-05）.
NASA CR-566 (PDF). [2008-08-15]. （原始内容存档 (PDF)于2008-06-24）.

Power Cycles. [2012-04-14]. （原始内容存档于2012-04-14）.
Huzel, D. K. and Huang, D. H. NASA SP-125, Design of Liquid Propellant Rocket Engines 2nd Edition. NASA. 1971 [2008-08-12]. （原始内容存档于2020-12-05）.
NASA CR-566 (PDF). [2008-08-15]. （原始内容存档 (PDF)于2008-06-24）.
Newsgroup correspondence （页面存档备份，存于互联网档案馆）, 1998-99