By William O. Criminale,Thomas Luther Jackson,Ronald Douglas Joslin
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Extra info for Theory and Computation of Hydrodynamic Stability Criminale
Typical results rlf this strdtegy results in an eigenvalue expression that has thc complex frequency as a function of the polar wave numlm, angle of obliquity, and thc Reynolds number if viscous forces are included. Or, because rlf the Sqlti~xtrar~sfnrmtionfrom the Cartesian to the polar wave number variables, the determination of thest: valucs can be made without resorting tr, the oblique angle value. If the behaviur for three-din~ensiunalityis dcsired, it can be inferred from the equivalent two-di mensictnal data by use of the transformation as was shown by Watson (1 960) or Betchov & Criininale (1 967).
196 I ) . Ch;tpter 2 is devoted to inviscid problems. 7 Gwmetries of relevance The mcan flows envisioned and described have been, at. least taciily, assumed to be those that are two-dirnensirsnal and unidirectional whether or no[ they are the true nr approximate s<,lutions to the Navier-Stokes equations. Undcr these restrictic~nsthis rnems thc channel, the flat plate boundary laycr r>rthe free shear flows of the jet, wakc. or mixing layer. Crwtesian cr~ordinatesdescribe these sitc~atinnsquite well.
Px = Re- 1V 2 VM LI, Henceforth, all variables will be assumed In be nnn-dimensional unlcss ntherwise noted. The parameter, Re, is che Reynr~ldsnumber, defined as It is extremely important. sfthe h 4 x s Climate orbiter. &LARS CT,IhIATE ORBITER TEAM FINDS 1,IKZLY CAUSE OF LOSSu A Fdi lure, to recognize and ct~rrectan error in 3 trat~sferof information bcturucn the Mars Climale Orbiter spacecraft [ e m in Colorado and the mission nrivigatiticrr~team in Califcjrnia led to the loss of thc spacecraft last week, prelin~inaryfindings by NASA's Jet.