An analysis of the acoustical and flowfield environment for the scaled 1-pound-force (lbf) thrust tabletop motor was performed. The jet characterization is based on computational fluid dynamics (CFD) in conjunction with Kirchhoff surface integral formulation and compared with correlations developed for measured rocket noise and a pressure fluctuation scaling (PFS) method. Comparisons are made for the overall sound pressure levels (OASPL's) and spectral dependence of sound pressure level (SPL).
Acoustical and Flowfield Characterization of a Tabletop Rocket Motor
9th International Congress on Sound and Vibration ; 2002 ; Orlando, FL, United States
2002-01-01
Preprint
No indication
English
Turbulent Transport in Rocket Motor Unsteady Flowfield
AIAA | 2000
|Small Rocket Flowfield Diagnostic Chambers
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