Computer program for design-point performance of turbojet and turbofan engine cycles

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035 ‡a(OCoLC)70824615
040 ‡aFER ‡cFER
049 ‡aUIUU
100 1 ‡aVanco, Michael R.
245 1 0 ‡aComputer program for design-point performance of turbojet and turbofan engine cycles / ‡cby Michael R. Vanco.
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], ‡c1967.
300 ‡a38 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical memorandum ; ‡vX-1340
500 ‡a"NASA TM X-1340."
500 ‡a"Lewis Research Center, Cleveland, Ohio."
500 ‡a"February 1967"--Cover.
504 ‡aIncludes bibliographical references (p. 38).
530 ‡aAlso available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 8/02/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19670009070_1967009070.pdf.
538 ‡aMode of access: Internet.
650 7 ‡aTurbojet engines. ‡2nasat
650 7 ‡aTurbofan engines. ‡2nasat
650 7 ‡aThermodynamics. ‡2nasat
650 7 ‡aThermodynamic cycles. ‡2nasat
650 7 ‡aPerformance. ‡2nasat
650 7 ‡aIBM 7040 computer. ‡2nasat
650 7 ‡aFortran. ‡2nasat
650 7 ‡aComputer programs. ‡2nasat
650 7 ‡aApplications programs (computers). ‡2nasat
710 2 ‡aLewis Research Center.
CID ‡a011424448
DAT 0 ‡a20101004084938.0 ‡b20141013010000.0
DAT 1 ‡a20141112173021.0 ‡b2018-03-07T19:53:44Z
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