1st Edition

Compressible Flow with Applications to Engines, Shocks and Nozzles

294 Pages 47 B/W Illustrations
by CRC Press

294 Pages 47 B/W Illustrations
by CRC Press

294 Pages 47 B/W Illustrations
by CRC Press

Compressible Flow with Application to Shocks and Propulsion is part of the series "Mathematics and Physics for Science and Technology", which combines rigorous mathematics with general physical principles to model practical engineering systems with a detailed derivation and interpretation of results. Volume V presents the mathematical theory of partial differential equations and methods of... Read more

2. Compressible Flow with Applications to Engines, Shocks and Nozzles
2.5 Equation of State and Thermodynamic Cycles.  2.6 Adiabatic Compressible Fluid Flow.  2.7. Vortex Sheet and the Normal Shock (Rankine 1870; Huginot 1887).  2.8. Oblique Shock (Busemann 1931) and Adiabatic Turn (Prandtl, Meyer 1908).  2.9. The "Choked" or "Shocked" Nozzle.  2.10. Conclusion.

Biography

Luis Manuel Braga da Costa Campos was Chair Professor and the Coordinator of the Scientific Area of Applied and Aerospace Mechanics in the Department of Mechanical Engineering and also the director (and founder) of the Center for Aeronautical and Space Science and Technology until retirement in 2020.

L.A. R. Vilela is currently completing an Integrated Master's degree in Aerospace Engineering at Institute Superior Tecnico (1ST) of Lisbon University.