LEADER 01743cam a2200433Ii 4500001    99118813653506421
005    20231117201806.0
006    m     o  d f
007    cr |||||||||||
008    200319e202003  ohua    obt  f000 0 eng d
035    on1145279742
035    (NjP)11881365-princetondb
035     |z(NjP)Voyager11881365
040    GPO |beng |erda |epn |cGPO |dMvI
049    DOCS
074    0830-H-14 (online)
086 0  NAS 1.26:2020-220489
090    Electronic Resource
100 1  Smith, Lance L., |eauthor.
245 10 Fuel flexible combustor for high-OPR compact-core N+3 propulsion engine : |bfinal technical report / |cLance L. Smith.
264  1 Cleveland, Ohio : |bNational Aeronautics and Space Administration, Glenn Research Center, |cMarch 2020.
300    1 online resource (91 pages) : |billustrations (mostly color).
336    text |btxt |2rdacontent
337    computer |bc |2rdamedia
338    online resource |bcr |2rdacarrier
490 1  NASA/CR ; |v2020-220489
500    "March 2020."
504    Includes bibliographical references (page 91).
536    Glenn Research Center |bNNC14CA30C
588    Description based on online resource, PDF version; title from title page (NASA, viewed on Mar. 19, 2020).
650  7 Bypass ratio. |2nasat
650  7 Computational fluid dynamics. |2nasat
650  7 Combustion chambers. |2nasat
650  7 High pressure. |2nasat
650  7 Dynamic tests. |2nasat
710 2  NASA Glenn Research Center, |eissuing body. |0http://id.loc.gov/authorities/names/no99028434
830  0 NASA contractor report ; |v2020-220489.
945    DOCS |cNAS 1.26:2020-220489
956 40  |uhttps://purl.fdlp.gov/GPO/gpo133808