
MAE 6530 Propulsion Systems II
Conical Supersonic Flow Fields
(Anderson, Chapter 6 pp. 239-260, Chapter 10, pp. 363-375

Lecture1 Notes: (html) ...................
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An Introduction to the Differential Conservation for Inviscid Flows
- Differential Form of Continuity Equation
- Divergence Theorem
- Differential Form of Momentum Equation
- Analog of Divergence Theorem
- Euler's Equation
- Energy Equation
- Crocco's Theorem
- Rotational and Irrotational Flow
Lecture2 Notes: (html) ...................
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Analysis of Supersonic Conical Flows
- Physical Aspects of Conical Flow
- Criterion for Irrotational Flow
- Spherical Coordinate System
- Continuity Equation for Conical Flow
- Crocco's Relation for Axi-symmetric Conical Flow
- Euler's Equation for Axi-symmetric Conical Flow
- Taylor-Maccoll Equation
- Numerical Procedure for Solving Axi-symmetric Conical Flow Field
- Boundary Value Problem Predictor/Corrector Equations
- Physical Aspects of Cone Flow (revisited)
- Qualitative Aspects of Conical Flow Fields at Angles of Attack
Cone-Flow Homework Problem Solution: (html) ..................
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Appendix I: NASA SP 3004 "Tables for Flow Around Right Circular Cones at Zero Angle of Attack"
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Appendix II: NASA SP 3007 "Tables for Flow Around Right Circular Cones at Small Angle of Attack"
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Appendix III: AXISYMMETRIC INLET DESIGN FOR COMBINED CYCLE ENGINES (pdf)
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