02541nam a2200457Ii 4500102892813MiAaHDL20250726000000.0m d cr bn ---auaua220428s1962 maua rbt f000 0 eng d(MiU)99187626099706381sdr-miu.99187626099706381(OCoLC)1312934979(GWLA)gwla on1312934979TRAALengrdaTRAALMAIND 301.45/4-3:62-639Sherman, Christopher,author.A two-fluid model for missile exhaust trail expansion /Christopher Sherman, A.W. Guess.Bedford, Massachusetts :Geophysics Research Directorate, Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force,1962.36 pages :illustrations ;28 cmtexttxtrdacontentunmediatednrdamediavolumencrdacarrierAFCRL-TR (Series) ;62-639Scientific report (Air Force Cambridge Research Laboratories (U.S.)) ;no. 4"GCA Technical Report 62-12-A.""1 June 1962."Includes bibliographic references (page 36).Contents: Derivation of two fluid equations; Discussion of the two fluid equations; The question of equilibrium, Asymptotic behavior of two-fluid equations for early and intermediate phases, Asymptotic behavior of the two-fluid equations for late phase, Conversion of two-fluid equations to a form suitable for machine calculations, Derivation of equations of mementum and energy from the Boltzmann equation, Derivation of collision frequency, mementum transfer, and energy transfer for a hard sphere model, Detail of derivation of energy transfer formula.Photocopy.Research supported by the Air Force Cambridge Research Laboratories, and performed by Geophysics Corporation of America, Bedford, Massachusetts, under contractAF 19(628)5617.Mode of access: Internet.Rocket enginesExhaust emissions.Condensation trails.Guided missiles.Guess, Arnold W.,1929-,author.Air Force Cambridge Research Laboratories (U.S.),issuing body.GCA Corporation,sponsor.Technical Report Archive & Image Library (TRAIL)3901510497582910289281320220802102015.020250726000000.020260310140653.02026-03-11T06:56:14Z2024-08-06T17:30:02ZSDR-MIUmiuALMAprepare.pl-004-009BKsdr-miu.99187626099706381MiUSDRGWLAmdp.39015104975829MIU99187626099706381MIUGWLA20260311googlemdp.390151049758291962pdbibUS fed doc