Linearized flow problems - Dr. K.P. Sinhamahapatra - Aero Dynamics - Lecture 14 of 43 - Video-lecture

Video-lecture, Aerospace Engineering

Description: High Speed Aero Dynamics by Dr. K.P. Sinhamahapatra, he tells us that Aerodynamicists disagree over the precise definition of hypersonic flow; minimum Mach numbers for hypersonic flow range from 3 to 12. Lecture14 of 43
Document information
Uploaded by: pierc
Views: 208
University: City University of New York (NY)
Address: Physics