Publication Date:
2018-06-06
Description:
The objective is to develop a coupled fluid/structure analysis tool for rocket turbopumps, advance hardware concepts and designs, and improve safety, reliability, and cost of space transportation.
Keywords:
Aircraft Propulsion and Power
Type:
2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting; 115-127; NASA/TM-2003-211896
Format:
application/pdf