The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 04, 2018

Filed:

Nov. 11, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Hao Shen, Maryland Heights, MO (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 7/60 (2006.01); G06F 17/10 (2006.01); G06F 17/50 (2006.01); B64C 30/00 (2006.01);
U.S. Cl.
CPC ...
G06F 17/5095 (2013.01); B64C 30/00 (2013.01); G06F 2217/82 (2013.01);
Abstract

A computer-implemented sonic boom prediction method for use in designing a supersonic aircraft is disclosed herein. The method includes receiving physical parameters and performance parameters for a supersonic aircraft, generating a three-dimensional (3D) flow field around the supersonic aircraft for at least one airspeed using a CFD model in a first region of a near field bounded by a first radial distance and a propagation model in a second region of the near field bounded by the first radial distance and the second radial distance. The 3D flow field generated by the CFD model is used as a boundary condition for the propagation model. The method further includes estimating sonic boom signatures on a ground surface using a long distance sonic boom propagation model that incorporates the 3D flow field estimated by the propagation model as an initial condition. The parameters are adjusted to reduce estimated sonic boom signatures.


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