Computation of Supersonic Flow over Flying Configurations / Adriana Nastase.
Material type: TextPublication details: Amsterdam, The Netherlands ; Boston, Mass. : Elsevier, c2008Edition: 1st edDescription: xvii, 389 p. : ill. (some col.) ; 25 cmISBN: 9780080449579 (hd.bd.); 0080449573 (hd.bd.)Subject(s): Aerodynamics, Supersonic -- Mathematical models | Boundary value problems | Navier-Stokes equationsDDC classification: 629.132305 LOC classification: TL571 | .N37 2008Item type | Current library | Call number | Copy number | Status | Date due | Barcode |
---|---|---|---|---|---|---|
Book | Karen | TL571 .N37 2008 (Browse shelf(Opens below)) | 1 | Available | 2020-1398 |
Includes bibliographical references and indexes.
Ch. 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 behaviors 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.
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