Computation of supersonic flow over flying configurations / Adriana Nastase

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 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