Supercritical Wing Sections III
In: Lecture Notes in Economics and Mathematical Systems 150
I. Introduction -- 1. Shockless Airfoils and Supercritical Wing Sections -- 2. Differential Equations of Gas Dynamics -- II. The Method of Complex Characteristics -- 1. A New Boundary Value Problem -- 2. Topology of the Paths of Integration -- 3. Iterative Scheme for the Map Function -- III. Transonic Airfoil Design Code -- 1. Isolated Airfoils -- 2. Compressor Cascades -- 3. Turbine Cascades -- 4. Comparison with Experiment -- IV. Two-Dimensional Analysis Code -- 1. Wave Drag -- 2. A Fast Solver -- 3. Remarks about Three-Dimensional Flow -- V. References -- VI. Users Manual for the Design Code -- 1. Introduction -- 2. The Input Deck -- 3. Closure -- 4. Achieving a Good Design -- 5. Boundary Layer Correction -- 6. Error Messages -- 7. Glossary of TAPE7 Parameters -- 8. Glossary of Output Parameters -- VII. Plots and Tables of Results -- 1. Airfoils Designed Using the New Code -- 2. Data from Analysis and Experiment -- VIII. Fortran Listings of the Codes -- 1. The New Design Code K -- 2. Update of the Analysis Code H.