Supercritical Wing Sections III
The purpose of this book is to survey computational flow research on the design and analysis of supercritical wing sections supported by the National Aeronautics and Space Administration at the Energy Research and Development Administration Mathematics and Computing Laboratory of New York University...
| Main Authors: | , , |
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| Format: | eBook |
| Language: | English |
| Published: |
Berlin, Heidelberg
Springer Berlin Heidelberg
1977, 1977
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| Edition: | 1st ed. 1977 |
| Series: | Lecture Notes in Economics and Mathematical Systems
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| Subjects: | |
| Online Access: | |
| Collection: | Springer Book Archives -2004 - Collection details see MPG.ReNa |
Table of Contents:
- 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.