CATALOG DATA:
Theoretical gas dynamics, including properties of compressible real fluids and fundamental relations for subsonic and supersonic flows.TEXTBOOK:
Anderson, John D., Modern Compressible Flow, McGraw-Hill Book Company, 1982.REFERENCES:
Zucrow, Maurice J. and Hoffman, Joe D., Gas Dynamics, Volume 1, John Wiley and Sons, Inc., 1976. Saad, Michael A., Compressible Fluid Flow, Prentice Hall, Inc., 1985.GOALS:
This course presents the fundamentals of classical compressible flow including real gas effects. Recent numerical approaches to the solution of practical problems are also discussed. Prerequisites:
Consent of instructor; thermodynamics, fluid dynamics, one-dimensional compressible flow.Topics:
- Two-dimensional steady flow: Oblique shock and expansion waves.
- Crocco's theorem.
- Linearized flows.
- Conical flow.
- Method of characteristics.
- Time-dependent finite difference techniques.
- Three-dimensional flow, transonic flow, hypersonic flow.
- High temperature gas projection.
- High temperature flows.
- Applications.
- Exams.
Computer Usage:
Design of a 2-D supersonic nozzle using method of characteristics; time-dependent, finite difference solution of 2-D supersonic nozzle flow or similar.ABET category content as estimated by faculty member who prepared the course description:
Engineering Science: 3 credits or 100%
Engineering Design: 0 creditsPrepared by: Professor Thomas J. Mueller
Last Update: March 27, 1992
Direct comments, questions, and corrections to amedept@nd.edu