000 01697nam a2200289 a 4500
001 000007104
005 20160221092659.0
008 070813s2003 xxuado grn 001 0 eng d
942 _c
020 _a9780072424430 (pasta dura)
020 _a0072424435 (pasta dura)
040 _aCO-BrUAC
041 0 _aeng
082 0 4 _221 ed.
_a629.132323
_bA545
100 1 _aAnderson, John David.,
_gJr.
_d1937-
245 1 0 _aModern compressible flow :
_bwith historical perspective /
_cJohn David Anderson, Jr.
250 _a3 ed.
260 _aBoston :
_bMcGraw Hill,
_c2003.
300 _a760 p. :
_bil., grafs., cuadros, diagrs., fot. byn, etc.
490 0 _aSeries in Aeronautical and Aerospase Engineering
505 0 _aCap. 1. Compressible flow - some history and introductory thoughts -- 2. Integral forms of the conservation equations for inviscid flows -- 3. One-dimensional flow -- 4. Oblique shock and expansion waves -- 5. Quasi-one dimensional flow -- 6. Differential conservation equations for inviscid flows -- 7. Unsteady wave motion -- 8. General conservation equations revisited: Velocity potential equation -- 9. Linearized flow -- 10. Conical flow -- 11. Numerical techniques for steady supersonic flow -- 12. The time-marching technique: With application to supersonic blunt bodies and nozzles -- 13. Three-dimensional flow -- 14. Transonic flow -- 15. Hypersonic flow -- 16. Properties of high-temperature gases -- 17. High-temperature flows: Basic examples.
544 1 _aDisponible en la Colección General
650 1 4 _aDinámica de Fluidos
650 1 4 _aDinámica de Gases
650 1 4 _aIngeniería Espacial
830 0 _aSeries in Aeronautical and Aerospase Engineering
999 _c7065
_d7065