Introduction to Compressible Flow
portes grátis
Introduction to Compressible Flow
Tang, Clement C.; Ames, Forrest E.
Taylor & Francis Ltd
07/2021
284
Dura
Inglês
9780367895679
15 a 20 dias
710
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1. Introduction.
2. Isentropic Flow.
3. Normal Shock Waves.
4. Oblique Shock Waves.
5. An Introduction to Prandtl-Meyer Flow.
6. Applications.
7. Linearized Flow.
8. Internal Compressible Flow with Friction.
9. Internal Compressible Flow with Heat Addition.
Appendix.
2. Isentropic Flow.
3. Normal Shock Waves.
4. Oblique Shock Waves.
5. An Introduction to Prandtl-Meyer Flow.
6. Applications.
7. Linearized Flow.
8. Internal Compressible Flow with Friction.
9. Internal Compressible Flow with Heat Addition.
Appendix.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
Mach Number;Supersonic Flow;Isentropic flow;Oblique Shock;Prandtl-Meyer flow;Normal Shock;Subsonic flow;Downstream Mach Number;Linearized flow;Total Pressure Loss;Fanno-line flow;Compressible Flow;Rayleigh line flow;Constant Area Duct;Conical flow;Normal Shock Wave;Free Stream Mach Number;Inlet Mach Number;Isentropic Mach Number;Total Pressure Ratio;Oblique Shock Wave;Inlet Total Temperature;Specific Heat Ratio;Convex Corner;Exit Mach Number;Prandtl Meyer Flow;Deflection Angle;Shock Tube;Supersonic Wind Tunnel;Moving Shock Wave;Control Volume Form
1. Introduction.
2. Isentropic Flow.
3. Normal Shock Waves.
4. Oblique Shock Waves.
5. An Introduction to Prandtl-Meyer Flow.
6. Applications.
7. Linearized Flow.
8. Internal Compressible Flow with Friction.
9. Internal Compressible Flow with Heat Addition.
Appendix.
2. Isentropic Flow.
3. Normal Shock Waves.
4. Oblique Shock Waves.
5. An Introduction to Prandtl-Meyer Flow.
6. Applications.
7. Linearized Flow.
8. Internal Compressible Flow with Friction.
9. Internal Compressible Flow with Heat Addition.
Appendix.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
Mach Number;Supersonic Flow;Isentropic flow;Oblique Shock;Prandtl-Meyer flow;Normal Shock;Subsonic flow;Downstream Mach Number;Linearized flow;Total Pressure Loss;Fanno-line flow;Compressible Flow;Rayleigh line flow;Constant Area Duct;Conical flow;Normal Shock Wave;Free Stream Mach Number;Inlet Mach Number;Isentropic Mach Number;Total Pressure Ratio;Oblique Shock Wave;Inlet Total Temperature;Specific Heat Ratio;Convex Corner;Exit Mach Number;Prandtl Meyer Flow;Deflection Angle;Shock Tube;Supersonic Wind Tunnel;Moving Shock Wave;Control Volume Form
