Development of an adaptive grid Navier-Stokes analysis method for rocket base flows-Reference-Cited by-同舟云学术

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Development of an adaptive grid Navier-Stokes analysis method for rocket base flows

Published:1988-07-11 Issue: Volume: Page:
ISSN:
Container-title:24th Joint Propulsion Conference
language:
Short-container-title:

Author:

HOLCOMB J.¹

Affiliation:

1. Boeing Aerospace Co., Seattle, WA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-2905

Reference19 articles.

1. Putnarn, L. E.,and Bissinger, N. C. "Resultsof AGARD Assessment of Prediction Capabilities for Nozzle Afterbody Flows." AIM-85-1464.

2. Hoffman, J. J., Birch, S. F., Hopcroft, R. G., and Holcomb, J. E. "Navier-Stokes Calculations of Rocket Base Flows," AIAA-87-0466.

3. Vcnkatapathy, E., and Lombard, C. K. "Accumtc Numerical Simulation of Supersonic let Exhaust Flow with CSCM on Adaptive Overlapping Grids," AIAA87-0465.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical investigation of exhaust plume radiative transfer phenomena;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13

2. Numerical investigation of twin-nozzle rocket plume phenomenology. II;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12

3. Numerical investigation of multi-plume rocket rhenomenology;33rd Joint Propulsion Conference and Exhibit;1997-07-06

4. Numerical investigation of twin-nozzle rocket plume phenomenology;35th Aerospace Sciences Meeting and Exhibit;1997-01-06

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