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020 _a9780080449579 (hd.bd.)
_cRM712.00
020 _a0080449573 (hd.bd.)
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_c200907131334
_drahah
_y06-01-2009
_zrasyilla
040 _aUKM
090 _aTL571
_b.N378
100 1 _aNastase, Adriana
245 1 0 _aComputation of supersonic flow over flying configurations /
_cAdriana Nastase
260 _aAmsterdam, The Netherlands :
_bElsevier,
_c2008
300 _axvii, 389 p. :
_bill. (some col.) ;
_c25 cm.
504 _aIncludes bibliographical references and indexes
505 0 _aCh. 1. Zonal, spectral solutions for the three-dimensional, compressible Navier-Stokes layer -- ch. 2. Hyperbolic potential boundary value problems of the axial disturbance velocities of outer flow, at NSL's edge -- ch. 3. Computation of axial disturbance velocities on wedged wings, in supersonic flow, at NSL's edge -- ch. 4. Computation of axial disturbance velocities on flying configurations with arbitrary shapes, in supersonic flow, at NSL's edge -- ch. 5. The aerodynamic characteristics of flying configurations with arbitrary shapes, in supersonic flow -- ch. 6. The visualization of the surfaces of pressure coefficients and aerodynamic characteristics of wedged delta and rectangular wings, in supersonic flow -- ch. 7. Qualitative analysis of the NSL's asymptotical behaviours in the vicinity of its critical zones -- ch. 8. Computation of the friction drag coefficients of the flying configurations -- ch. 9. Inviscid and viscous aerodynamical global optimal design -- ch. 10. Comparison of the theoretical aerodynamic characteristics of wing models with experimental determined results
650 0 _aAerodynamics, Supersonic
_xMathematical models
650 0 _aBoundary value problems
650 0 _aNavier-Stokes equations
_960500
907 _a.b14494243
_b2020-10-15
_c2019-11-12
942 _c01
_n0
_kTL571 .N378
914 _avtls003408914
990 _arab
991 _aJabatan Komputeran Industri -TKI
998 _at
_b2009-01-06
_cm
_da
_feng
_gne
_y0
_z.b14494243
999 _c441854
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