Refined Tetrahedral Meshes with Mach Cone Aligned Prisms for Sonic Boom Analysis

Journal of Aircraft ◽

10.2514/1.c031943 ◽

2013 ◽

Vol 50 (3) ◽

pp. 778-790 ◽

Author(s):

Susan E. Cliff ◽

Alaa A. Elmiligui ◽

Richard L. Campbell ◽

Scott D. Thomas

Keyword(s):

Tetrahedral Meshes

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Evaluation of Refined Tetrahedral Meshes with Projected, Stretched, and Sheared Prism Layers for Sonic Boom Analysis (Invited)

29th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2011-3338 ◽

2011 ◽

Author(s):

Susan Cliff ◽

Alaa Elmiligui ◽

Richard Campbell ◽

Scott Thomas

Keyword(s):

Tetrahedral Meshes

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MODELING OF SONIC BOOM WAVE PROPAGATION THROUGH TURBULENCE

TsAGI Science Journal ◽

10.1615/tsagiscij.v42.i3.10 ◽

2011 ◽

Vol 42 (3) ◽

pp. 275-288

Author(s):

Sergei L. Chernyshev

Keyword(s):

Wave Propagation ◽

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Sonic boom propagation from maneuvering aircraft

10.2514/6.1969-1134 ◽

1969 ◽

Author(s):

R. HAEFELI

Keyword(s):

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Effect of SST operational maneuvers on sonic boom

10.2514/6.1972-196 ◽

1972 ◽

Author(s):

G. HAGLUND ◽

E. KANE

Keyword(s):

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Adaptive inviscid flow solutions for aerospace geometries on efficiently generated unstructured tetrahedral meshes

10.2514/6.1993-3390 ◽

1993 ◽

Author(s):

N. WEATHERILL ◽

O. HASSAN ◽

M. MARCHANT ◽

D. MARCUM

Keyword(s):

Inviscid Flow ◽

Tetrahedral Meshes ◽

Unstructured Tetrahedral Meshes

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Optimization procedure for reduced sonic boom in high speed flight

10.2514/6.1995-2156 ◽

1995 ◽

Author(s):

A Chattopadhyay ◽

J Narayan ◽

N Pagaldipti ◽

X Wensheng ◽

S Cheung

Keyword(s):

Optimization Procedure ◽

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Problems in sonic boom theory studied as issues of singular perturbation

10.2514/6.1996-2165 ◽

1996 ◽

Author(s):

H. Cheng ◽

C. Lee

Keyword(s):

Singular Perturbation ◽

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Sonic-Boom Prediction of a Scaled Low-Boom Demonstration Aircraft Considering Viscosity Effects

29th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2011-3662 ◽

2011 ◽

Author(s):

Hiroaki Ishikawa ◽

Y. Makino ◽

K. Ohira

Keyword(s):

Viscosity Effects

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Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design

AIAA Scitech 2021 Forum ◽

10.2514/6.2021-1009 ◽

2021 ◽

Author(s):

Yusuf Demiroglu ◽

Sihmehmet Yildiz ◽

Melike Nikbay

Keyword(s):

Shape Design ◽

Supersonic Aircraft

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DLR TAU Simulations for the Third AIAA Sonic Boom Prediction Workshop Near-Field Cases

AIAA Scitech 2021 Forum ◽

10.2514/6.2021-0472 ◽

2021 ◽

Author(s):

Jochen Kirz

Keyword(s):

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