Documents in the NTIS Technical Reports collection are the results of federally funded research. They are directly submitted to or collected by NTIS from Federal agencies for permanent accessibility to industry, academia and the public.  Before purchasing from NTIS, you may want to check for free access from (1) the issuing organization's website; (2) the U.S. Government Printing Office's Federal Digital System website; (3) the federal government Internet portal; or (4) a web search conducted using a commercial search engine such as
Accession Number N14-0004249
Title Coupled Fluid-Structure Interaction Analysis of Solid Rocket Motor with Flexible Inhibitors.
Publication Date Jan 2014
Media Count 18p
Personal Author H. Q. Yang J. West R. Harris
Abstract No abstract available.
Keywords Computational fluid dynamics
Flow distribution
Internal flow
Pressure oscillations
Solid propellant rocket engines
Sound pressure
Space shuttles
Unsteady flow
Vortex shedding

Source Agency National Aeronautics and Space Administration
NTIS Subject Category 46B - Fluid Mechanics
51A - Aerodynamics
Corporate Author National Aeronautics and Space Administration, Huntsville, AL. George C. Marshall Space Flight Center.
Document Type Technical report
Title Note N/A
NTIS Issue Number 1421
Contract Number NNM12AA41C

Science and Technology Highlights

See a sampling of the latest scientific, technical and engineering information from NTIS in the NTIS Technical Reports Newsletter

Acrobat Reader Mobile    Acrobat Reader