by Frances Bauer, Paul Garabedian, David Korn, Antony Jameson
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.
