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181   $ctxt
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183   $acr
200 00$aLiquid rocket engine combustion instability /$fedited by  William E. Anderson and Vigor Yang
205   $a1st ed.
210   $aWashington, D.C. $cAmerican Institute of Aeronautics and Astronautics, Inc.$d1995
215   $a1 online resource (580 p.)
225 1 $aProgress in astronautics and aeronautics ;$vv. 169
300   $aDescription based upon print version of record.
311 08$a1-56347-183-3 
320   $aIncludes bibliographical references and index.
327   $apt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology.
330   $aSince the invention of the V-2 rocket during World War II, combustion instabilities have been recognized as one of the most difficult problems in the development of liquid propellant rocket engines. This book is the first published in the United States on the subject since NASA's Liquid Rocket Combustion Instability (NASA SP-194) in 1972. In this book, experts cover four major subject areas: engine phenomenology and case studies, fundamental mechanisms of combustion instability, combustion instability analysis, and engine and component testing. Especially noteworthy is the inclusion of technical information from Russia and China--a first.
410  0$aProgress in astronautics and aeronautics ;$vv. 169.
606   $aLiquid propellant rockets
606   $aRocket engines$xCombustion
615  0$aLiquid propellant rockets.
615  0$aRocket engines$xCombustion.
676   $a629.47522
701   $aYoung$b Vigor$01867862
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906   $aBOOK
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996   $aLiquid rocket engine combustion instability$94475608
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