Rapid Prediction of Low-Boom and Aerodynamic Performance of Supersonic Transport Aircraft Using Panel Methods

Rapid Prediction of Low-Boom and Aerodynamic Performance of Supersonic Transport Aircraft Using Panel Methods

The Utah State University Aerolab developed and tested a set of tools for rapid prediction of the loudness of a sonic boom generated by supersonic transport aircraft. This work supported a larger effort led by Texas A&M to investigate the use of adaptive aerostructures in lowering sonic boom lou...

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Bibliographic Details
Main Author: Giblette, Ted N.
Format: Others
Published: DigitalCommons@USU 2019
Subjects:
panel methods
sonic boom
class-shape transformations
PANAIR
supersonic
PyLdB
Mechanical Engineering
Online Access:https://digitalcommons.usu.edu/etd/7603
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=8736&context=etd

Internet

https://digitalcommons.usu.edu/etd/7603
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=8736&context=etd

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