A Multi-Fidelity Prediction of Aerodynamic and Sonic Boom Characteristics of the JAXA Wing Body

Author:

Carpenter Forrest L.1,Cizmas Paul1,Bolander Christian R.2,Giblette Ted N.2,Hunsaker Douglas F.2

Affiliation:

1. Texas A&M University

2. Utah State University

Publisher

American Institute of Aeronautics and Astronautics

Reference39 articles.

1. Numerical Simulations of a Quiet SuperSonic Technology (QueSST) Aircraft Preliminary Design

2. Magee, T. E., Fugal, S. R., Fink, L. E., Adamson, E. E., and Shaw, S. G. “System-Level Experimental Validations for Supersonic Commercial Transport Aircraft Entering Service in the 2018-2020 Time Period: Phase II Final Report,” Technical Report NASA/CR-2015-218983, NASA Langley Research Center, 2015.

3. Morgenstern, J., Buonanno, M., Yao, J., Murugappan, M., Paliath, U., Cheung, L., Ramakrishnan, I. M. K., Pastouchenko, N., and Wood, T. “Advanced Concept Studies for Supersonic Commercial Transports Entering Service in the 2018-2020 Period Phase 2,” Technical Report NASA/CR-2015-218719, NASA Langley Research Center, 2015.

4. Maglieri, D. J., Bobbitt, P. J., Plotkin, K. J., Shepherd, K. P., Coen, P. G., and Richwine, D. M. “Sonic Boom: Six Decades of Research,” Technical Report NASA/SP-2014-622, NASA Langley Research Center, 2014.

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