John Bussoletti

Experienced CFD Developer and Leader of Development Team Focused On Development Accurate Modeling Tools For Aircraft Development

Bonney Lake, Washington, United States of America

Research Expertise

Computational Fluid Dynamics

Computational Electrormagnetics

Software Development

High Performance Computing

About

John Bussoletti is an experienced physicist and researcher with a strong background in experimental nuclear physics. He received his AB in Physics from Princeton in 1972 and went on to earn his PhD in Physics (Experimental Nuclear Physics) from University of Washington in 1978. After completing his education, Bussoletti began his career as a Research Engineer at Boeing, where he has worked for several years. He has a strong understanding of mathematical and scientific principles, as well as experience in conducting experiments and analyzing data. He has a long history of both developing and leading teams for developing computational modeling tools to support engineering design. Bussoletti is dedicated to advancing the field of physics through his research and is always seeking new challenges and opportunities to expand his knowledge and expertise.

Legacy Map

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Publications

Numerical Evidence of Multiple Solutions for the Reynolds-Averaged Navier-Stokes Equations for High-Lift Configurations

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

2013

Observations Regarding Algorithms Required for Robust CFD Codes

Mathematical Modelling of Natural Phenomena

2011

Algorithm Issues and Challenges Associated with the Development of Robust CFD Codes

Variational Analysis and Aerospace Engineering

2009

Aerodynamic Characteristics of Bodies of Revolution at Near-Sonic Speeds

Journal of Aircraft

2007

Pressures and Drag Characteristics of Bodies of Revolution at Near Sonic Speeds Including the Effects of Viscosity and Wind Tunnel Walls

45th AIAA Aerospace Sciences Meeting and Exhibit

2007

Minimizing CFD Uncertainty for Commercial Aircraft Applications (Invited)

41st Aerospace Sciences Meeting and Exhibit

2003

Effect of wind tunnel walls on the flutter characteristics of an airplane model

19th AIAA Applied Aerodynamics Conference

2001

An optimal reduced-order aeroelasltic modeling based on a response-based modal analysis of unsteady CFD models

19th AIAA Applied Aerodynamics Conference

2001

CFD studies in support of NWTC test section design

35th Aerospace Sciences Meeting and Exhibit

1997

CFD calibration and validation - The challenges of correlating computational model results with test data

25th Plasmadynamics and Lasers Conference

1994

Practical Design and Optimization in Computational Fluid Dynamics

23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference

1993

Using a full potential solver for propulsion system exhaust simulation

Journal of Propulsion and Power

1993

An adaptive grid method for analysis of 3D aircraft configurations

Computer Methods in Applied Mechanics and Engineering

1992

Computations of the supersonic flow over an HSCT type configuration and comparison with wind tunnel data

9th Applied Aerodynamics Conference

1991

A locally refined rectangular grid finite element method: Application to computational fluid dynamics and computational physics

Journal of Computational Physics

1991

Application of computational methods in aeroacoustics

13th Aeroacoustics Conference

1990

Solution Adaptive Local Rectangular Grid Refinement for Transonic Aerodynamic flow Problems

Proceedings of the Eighth GAMM-Conference on Numerical Methods in Fluid Mechanics

1990

Application of Sparse Matrix Solvers as Effective Preconditioners

SIAM Journal on Scientific and Statistical Computing

1989

TranAir Technology: Solutions for Large PDE Problems

Solution of Superlarge Problems in Computational Mechanics

1989

Transonic analysis of arbitrary configurations using locally refined grids

11th International Conference on Numerical Methods in Fluid Dynamics

TRANAIR - A computer code for transonic analyses of arbitrary configurations

25th AIAA Aerospace Sciences Meeting

1987

An Exterior Poisson Solver Using Fast Direct Methods and Boundary Integral Equations with Applications to Nonlinear Potential Flow

SIAM Journal on Scientific and Statistical Computing

1986

A transonic rectangular grid embedded panel method

3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference

1982

Investigation of the electric quadrupole strength in 13N using the reaction

Nuclear Physics A

1980

Isospin-forbidden β-decay of 28Mg

Nuclear Physics A

1978

Radiative transitions and isospin mixing inC12

Physical Review C

1977

Application of the Direct-Semidirect Model to the Interpretation ofE1andE2Strength inC14(ppol,γ0)N

Physical Review Letters

1976

Application of the Direct-Semidirect Model to the Interpretation ofE1andE2Strength inC14(ppol,γ0)N

Physical Review Letters

1976

Isospin mixing in 12C

Physics Letters B

1976

Analyzing Power for Elastic Scattering of Protons from 13C

Experientia Supplementum

1976

Large Isospin-Mixing Matrix Element inC12

Physical Review Letters

1972

Education

University of Washington

PhD, Physics (Experimental Nuclear Physics) / June, 1978

Seattle, Washington, United States of America

Princeton University

AB, Physics / June, 1972

Princeton, New Jersey, United States of America

Experience

Boeing

Research Engineer / June, 1977 — March, 2015

Computational Fluid Dynamic Development

HCL America

Program Developer / April, 2015 — December, 2019

Ladon Robotics

CFD Consultant / April, 2022 — October, 2023

Links & Social Media

Linked In Profile

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