Abstract The technology of propulsive systems draws on a substantial body of formal fluid mechanical theory. The design of exhaust nozzles, turbine and compressor blade cascades, the analysis of the design-point operation of subsonic and supersonic inlets, etc., involve mathematically sophisticated solutions of the fluid motion and aero-thermochemical coupling between it and the medium. As difficult as some of these problems are, their basic formulation is usually reasonable clear. With enough effort, a theoretical framework can be developed and extended by controlled experimental work.
Interaction Flows Due to Supersonic Secondary Jets
Jet, Rocket, Nuclear, Ion and Electric Propulsion ; 6 ; 487-507
Applied Physics and Engineering ; 7 , 6
01.01.1968
21 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Penetration of Gaseous Jets In Supersonic Flows
AIAA | 2006
|Penetration of Gaseous Jets in Supersonic Flows
AIAA | 2006
|