Exact Beltramian solutions for hemispherically bounded cyclonic flowfields

Author:

Williams Langston L.1ORCID,Majdalani Joseph1ORCID

Affiliation:

1. Department of Aerospace Engineering, 211 Davis Hall, Auburn University, Auburn, Alabama 36849-5338, USA

Funder

National Science Foundation

Sierra Nevada Corporation

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Reference46 articles.

1. W. H. Knuth , P. A. Bemowski , D. J. Gramer , J. Majdalani , and W. J. Rothbauer , “ Gas-Fed, Vortex Injection Hybrid Rocket Engine,” SBIR Phase I, NASA Final Technical Contract No. NAS8-40679 ( Orbital Technologies Corporation, Madison, Wisconsin, 1996).

2. W. H. Knuth , M. J. Chiaverini , D. J. Gramer , and J. A. Sauer , “ Final Report on Vortex Combustion Ramjet—A Phase I SBIR Project,” SBIR Phase I, NASA Final Technical Contract Nos. NAS3-99039 and OTC-GS075-FR-99-1 ( Orbital Technologies Corporation, Madison, Wisconsin, 1999).

3. Study of Flame Stability in a Step Swirl Combustor

4. V. Katta and W. Roquemore , “ Numerical studies of trapped-vortex combustor,” AIAA Paper No. 96-2660, 1996.

5. M. J. Chiaverini , J. A. Sauer , and W. H. Knuth , “ Final Report on Vortex Com-bustion Combined Cycle Engine—A Phase I SBIR Project,” AFRL Contract Nos. F04611-99-C-0063 and OTC-GS082-FR-99-1 ( Orbital Technologies Corporation, Madison, Wisconsin, 1999).

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