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Description
High Speed Aerodynamics. Instructor: Prof. K. P. Sinhamahapatra, Department of Aerospace Engineering, IIT Kharagpur.
The course introduces the fundamental concepts and principles of compressible flow and intends to provide the necessary background for advanced studies on the subject. A number of application problems are incorporated to illustrate the concepts. The course covers the general principles and essentials of compressible flow, the flow equations, one-dimensional gas dynamics, wave motion and waves in supersonic flow, flow in ducts, small-perturbation theory, method of characteristics and similarity rules. The exercises included in the course are intended to demonstrate the use of the course material and to outline additional equations and results. Even though the course is prepared mainly for the use of undergraduate students in aerospace engineering, it will also be useful to graduate students, teachers and practicing engineers and scientists (from nptel.ac.in)
Course Curriculum
- Lecture 01 – Introduction and Review of Thermodynamics Unlimited
- Lecture 02 – Review of Thermodynamics Unlimited
- Lecture 03 – Second Law of Thermodynamics Unlimited
- Lecture 04 – Some Useful Topics in Thermodynamics for High Speed Aerodynamics Unlimited
- Lecture 05 – One-dimensional Gas Dynamics Unlimited
- Lecture 06 – One-dimensional Gas Dynamics (cont.) Unlimited
- Lecture 07 – One-dimensional Gas Dynamics (cont.) Unlimited
- Lecture 08 – One-dimensional Waves Unlimited
- Lecture 09 – One-dimensional Waves (cont.) Unlimited
- Lecture 10 – One-dimensional Waves (cont.) Unlimited
- Lecture 11 – Waves and Supersonic Flow: Oblique Shock Relations Unlimited
- Lecture 12 – Waves and Supersonic Flow: Weak Shocks and Mach Waves Unlimited
- Lecture 13 – Waves and Supersonic Flow: Supersonic Expansion by Turning Unlimited
- Lecture 14 – Waves and Supersonic Flow (cont.) Unlimited
- Lecture 15 – Shock Expansion Theory Unlimited
- Lecture 16 – Flow through Ducts and Channels Unlimited
- Lecture 17 – Flow through Converging and Converging-Diverging Ducts Unlimited
- Lecture 18 – Flow in Converging-Diverging Nozzles Unlimited
- Lecture 19 – Adiabatic Flow in Ducts with Friction Unlimited
- Lecture 20 – Adiabatic Flow in Ducts with Friction (cont.) Unlimited
- Lecture 21 – Isothermal Flow in Ducts with Friction Unlimited
- Lecture 22 – Flow in Uniform Duct with Heating Unlimited
- Lecture 23 – Multi-dimensional Flow Problems Unlimited
- Lecture 24 – Multi-dimensional Flow Problems (cont.) Unlimited
- Lecture 25 – Linearized Flow Problems Unlimited
- Lecture 26 – Linearized Flow Problems: Ackeret’s Problem Unlimited
- Lecture 27 – Linearized Flow Problems: Supersonic Flow over a Wavy Wall Unlimited
- Lecture 28 – Linearized Flow Problems: Supersonic Flow over Wings Unlimited
- Lecture 29 – Linearized Flow Problems: Pressure Coefficient Unlimited
- Lecture 30 – Linearized Supersonic Flow Problems: Potential Function Unlimited
- Lecture 31 – Linearized Flow Problems: Non-axisymmetric Flow over a Body of Revolution Unlimited
- Lecture 32 – Linearized Problems – Forces on Slender Bodies Unlimited
- Lecture 33 – Linearized Problems – Forces on Slender Bodies (cont.) Unlimited
- Lecture 34 – Similarity Rules for High Speed Flows Unlimited
- Lecture 35 – Similarity Rules for High Speed Flows (cont.) Unlimited
- Lecture 36 – Similarity Rules for High Speed Flows (cont.) Unlimited
- Lecture 37 – Similarity Rule in Hypersonic Flow Unlimited
- Lecture 38 – Transonic Flow Unlimited
- Lecture 39 – Transonic Flow (cont.) Unlimited
- Lecture 40 – Transonic Flow (cont.) Unlimited
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