Computation of Supersonic Flow over Flying ConfigurationsBy
- Adriana Nastase, Aerodynamik des Fluges, University of Technology RWTH, Aachen, Germany
University libraries and departmental/institute libraries, space centres such as NASA, DLR, DGLR, ONERA, FOI, ESA etc. American Institute of Physics; Association Francaise de Mechanique; Corporate aerospace companies such as Boeing, Airbus etc.
Hardbound, 410 Pages
Published: December 2007
- Chapter 1. Zonal, Spectral Solutions for the Three-Dimensional, Compressible Navier-Stokes LayerChapter 2. Hyperbolic Potential Boundary Value Problems of the Axial Disturbance Velocities of Outer Flow, at NSL's EdgeChapter 3. Computation of Axial Disturbance Velocities on Wedged Wings, in Supersonic Flow, at NSL's EdgeChapter 4. Computation of Axial Disturbance Velocities on Flying Configurations with Arbitrary Shapes, in Supersonic Flow, at NSL's EdgeChapter 5. The Aerodynamic Characteristics of Flying Configurations with Arbitrary Shapes, in Supersonic FlowChapter 6. The Visualization of the Surfaces of Pressure Coefficients and Aerodynamic Characteristics of Wedged Delta and Rectangular Wings, in Supersonic FlowChapter 7. Qualitative Analysis of the NSL's Asymptotical Behaviours in the Vicinity of its Critical ZonesChapter 8. Computation of the Friction Drag Coefficients of the Flying ConfigurationsChapter 9. Inviscid and Viscous Aerodynamical Global Optimal DesignChapter 10. Comparison of the Theoretical Aerodynamic Characteristics of Wing Models with Experimental Determined ResultsFinal RemarksBook PresentationOutlookSubject IndexAuthor Index