aero lab 5
Chp%3 a10.1007%2f978 3-642-55753-8-3
LAB 4 aircraft design
1 The University of Manchester Aero-Physics Laboratory Compressible Vortex Rings in a Shock Tube with Helium Driver R. Mariani Prof. K. Kontis.
Combustion Team Supersonic Combustion 6/12/20151NASA Grant URC NCC NNX08BA44A Faculty Advisors: Dr. Guillaume Dr. Wu Dr. Boussalis Dr. Liu Dr. Rad Sara.
An Accuate and Rapid Method for the Design of Super Sonice Nozzles
