An efficient strategy for propagating sonic boom signatures from a near-field Computational Fluid Dynamics (CFD) solution to the mid-field is presented. The method is based on a high-order accurate finite-difference discretization of the 3D Euler equations on a specially designed curvilinear grid and a single sweep space marching solution algorithm. The new approach leads to more than a factor of two reduction in overall computational resources compared to the current method used to propagate near-field sonic booms to the ground. Accuracy and efficiency of the near-field to mid-field process is demonstrated using a selection of test cases from the AIAA Sonic Boom Prediction Workshops. Azimuthal dependence of nonlinear wave propagation from ...
This paper presents an accurate approach to simulate the sonic boom of a supersonic aircraft. The ne...
Numerical method for calculating near field sonic room pressure signatures and application to high s...
An improvement in sonic boom extrapolation techniques has been the desire of aerospace designers for...
A 3-D parabolized Navier-Stokes (PNS) code was used to calculate the supersonic overpressures from t...
Presented at the 24th AIAA Applied Aerodynamics Conference, San Francisco, California, June 5-8, 200...
The sonic boom is one of the most severe problems confronting the advancement of high-speed air tran...
International audienceThis paper presents an accurate approach to simulate the sonic boom of superso...
This paper first describes the numerical simulation and shape optimization of the Lockheed SEEB-ALR ...
Automated, parallelized, time-efficient surface definition and grid generation and flow simulation m...
As the industry progresses towards realizing a commercial supersonic aircraft, the push to reduce no...
A new approach for the inclusion of Computational Fluid Dynamics flow solutions into predicting soni...
Sonic Booms of two different bodies, a double cone configuration and a modified F-5E aircraft are pr...
This paper describes the NASA ARC program in sonic boom prediction methodologies. This activity supp...
NASA created the Supersonics Project as part of the NASA Fundamental Aeronautics Program to advance ...
Calculations of shock wave pattern in field surrounding arbitrary aircraft configurations at superso...
This paper presents an accurate approach to simulate the sonic boom of a supersonic aircraft. The ne...
Numerical method for calculating near field sonic room pressure signatures and application to high s...
An improvement in sonic boom extrapolation techniques has been the desire of aerospace designers for...
A 3-D parabolized Navier-Stokes (PNS) code was used to calculate the supersonic overpressures from t...
Presented at the 24th AIAA Applied Aerodynamics Conference, San Francisco, California, June 5-8, 200...
The sonic boom is one of the most severe problems confronting the advancement of high-speed air tran...
International audienceThis paper presents an accurate approach to simulate the sonic boom of superso...
This paper first describes the numerical simulation and shape optimization of the Lockheed SEEB-ALR ...
Automated, parallelized, time-efficient surface definition and grid generation and flow simulation m...
As the industry progresses towards realizing a commercial supersonic aircraft, the push to reduce no...
A new approach for the inclusion of Computational Fluid Dynamics flow solutions into predicting soni...
Sonic Booms of two different bodies, a double cone configuration and a modified F-5E aircraft are pr...
This paper describes the NASA ARC program in sonic boom prediction methodologies. This activity supp...
NASA created the Supersonics Project as part of the NASA Fundamental Aeronautics Program to advance ...
Calculations of shock wave pattern in field surrounding arbitrary aircraft configurations at superso...
This paper presents an accurate approach to simulate the sonic boom of a supersonic aircraft. The ne...
Numerical method for calculating near field sonic room pressure signatures and application to high s...
An improvement in sonic boom extrapolation techniques has been the desire of aerospace designers for...