Lecture notes in economics and mathematical systems, 108.
GENERAL NOTES
Text of Note
Bd 1 u.d.T.: A theory of supercritical wing sections, with computer programms and examples.
CONTENTS NOTE
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I. Theory.- 1. Introduction.- 2. Models of Shock Structure.- 3. Iterative Schemes for Three Dimensional Analysis.- 4. Choice of Coordinates and Conformal Mapping.- 5. Two Dimensional Analysis with a Turbulent Boundary Layer Correction.- 6. Design in the Hodograph Plane: A New Model of the Trailing Edge.- 7. Design in the Hodograph Plane: Choice of Parameters.- 8. Bibliography.- II. Data.- 1. Catalog of Transonic Airfoils.- 2. Evaluation of Analysis Methods.- 3. Comparison of Experimental Data with the Boundary Layer Correction.- 4. Comparison of Experimental Data with the Boundary Layer Correction Using the Quasiconservation Option.- 5. Drag Polars.- 6. Schlieren Photographs.- III. Fortran Programs.- 1. Operation of the Turbulent Boundary Layer Correction Program H.- 2. Glossaries and Tables for Program H..- 3. Operation of the Three Dimensional Analysis Program J.- 4. Glossary and Table for Program J.- 5. Listing of the Boundary Layer Analysis Program H.- 6. Listing of the Three Dimensional Analysis Program J.- 7. Listing of Quasiconservation Option for Program H.- 8. Listing of Update for Design Programs B and D.