NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Cartesian Mesh Simulations for the Third AIAA Sonic Boom Prediction WorkshopSimulation results are presented for all cases from the Third AIAA Sonic Boom Prediction Workshop. An inviscid, embedded-boundary Cartesian-mesh flow solver is used in conjunction with adjoint-based mesh adaptation to compute nearfield pressure signatures. Specialized techniques are applied to maximize accuracy and minimize cost on Cartesian meshes. The Richardson-based error estimate highlights regions of the signatures most sensitive to mesh refinement. Timing results and coarse, medium, and fine mesh sizes for nearfield cases demonstrate that the parallel decomposition approach is efficient in both computational time and wall-clock. Pressure signals are propagated to the ground using an augmented Burgers’ equation solver to predict boom carpets. Ground signatures and loudness metrics are presented for a standard atmosphere as well as more realistic atmospheric profiles, which affect overall noise levels and can significantly widen the boom carpet. Mesh convergence studies show that high sampling frequencies, around 500 kHz, are required for propagation, and the sampling frequency increases at large off-track angles with longer acoustic ray paths and propagation times. The numerical methods yield accurate results for predicting low sonic boom signatures while being among the least computationally expensive of the workshop.
Document ID
20205011380
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Wade M. Spurlock
(Science and Technology Corporation (United States) Hampton, Virginia, United States)
Michael J. Aftosmis
(Ames Research Center Mountain View, California, United States)
Marian Nemec
(Ames Research Center Mountain View, California, United States)
Date Acquired
December 9, 2020
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AIAA SciTech Forum
Location: Virtual
Country: US
Start Date: January 11, 2021
End Date: January 21, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 110076.02.01.03.31
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
ARMD
CST
No Preview Available