Sonic boom predictions using a solution-adaptive full-potential code-Reference-Cited by-同舟云学术

Sonic boom predictions using a solution-adaptive full-potential code

Published:1994-01 Issue:1 Volume:31 Page:57-63
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Madson Michael D.¹

Affiliation:

1. NASA Ames Research Center, Moffett Field, California 94035

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.46455

Reference17 articles.

1. 'Johnson, F. T., Samant, S. S., Bieterman, M. B., Melvin, R. G., Young, D. P., Bussoletti, J. E., and Hilmes, C. L. "TRANAIR: A Full-Potential, Solution-Adaptive Rectangular Grid Code for Predicting Subsonic, Transonic, and Supersonic Flows About Arbitrary Configurations (Theory Document)," NASA CR-4348, Dec.1992.

2. 2Johnson, F. T., Samant, S. S., Bieterman, M. B., Melvin, R. G., Young, D. P., Bussoletti, J. E., and Hilmes, C. L. "TRANAIR: A Full-Potential, Solution-Adaptive Rectangular Grid Code for Predicting Subsonic, Transonic, and Supersonic Flows About Arbitrary Configurations (User Guide)," NASA CR-4349, Dec.1992.

3. Transonic analysis of the F-16A with under-wing fuel tanks - An application of the TranAir full-potential code

4. TranAir and Euler computations of a generic fighter including comparisons with experimental data

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