High Speed Aerodynamics (Prof. K. P. Sinhamahapatra, IIT Kharagpur) | Aeronautics and Astronautics

High Speed Aerodynamics

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)

Introduction and Review of Thermodynamics

Lecture 01 - Introduction and Review of Thermodynamics

Lecture 02 - Review of Thermodynamics

Lecture 03 - Second Law of Thermodynamics

Lecture 04 - Some Useful Topics in Thermodynamics for High Speed Aerodynamics

Lecture 05 - One-dimensional Gas Dynamics

Lecture 06 - One-dimensional Gas Dynamics (cont.)

Lecture 07 - One-dimensional Gas Dynamics (cont.)

Lecture 08 - One-dimensional Waves

Lecture 09 - One-dimensional Waves (cont.)

Lecture 10 - One-dimensional Waves (cont.)

Lecture 11 - Waves and Supersonic Flow: Oblique Shock Relations

Lecture 12 - Waves and Supersonic Flow: Weak Shocks and Mach Waves

Lecture 13 - Waves and Supersonic Flow: Supersonic Expansion by Turning

Lecture 14 - Waves and Supersonic Flow (cont.)

Lecture 15 - Shock Expansion Theory

Lecture 16 - Flow through Ducts and Channels

Lecture 17 - Flow through Converging and Converging-Diverging Ducts

Lecture 18 - Flow in Converging-Diverging Nozzles

Lecture 19 - Adiabatic Flow in Ducts with Friction

Lecture 20 - Adiabatic Flow in Ducts with Friction (cont.)

Lecture 21 - Isothermal Flow in Ducts with Friction

Lecture 22 - Flow in Uniform Duct with Heating

Lecture 23 - Multi-dimensional Flow Problems

Lecture 24 - Multi-dimensional Flow Problems (cont.)

Lecture 25 - Linearized Flow Problems

Lecture 26 - Linearized Flow Problems: Ackeret's Problem

Lecture 27 - Linearized Flow Problems: Supersonic Flow over a Wavy Wall

Lecture 28 - Linearized Flow Problems: Supersonic Flow over Wings

Lecture 29 - Linearized Flow Problems: Pressure Coefficient

Lecture 30 - Linearized Supersonic Flow Problems: Potential Function

Lecture 31 - Linearized Flow Problems: Non-axisymmetric Flow over a Body of Revolution

Lecture 32 - Linearized Problems - Forces on Slender Bodies

Lecture 33 - Linearized Problems - Forces on Slender Bodies (cont.)

Lecture 38 - Transonic Flow

Lecture 39 - Transonic Flow (cont.)

Lecture 40 - Transonic Flow (cont.)

References

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.