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Anthony Paul Haas
Anthony Paul Haas
Los Alamos National Laboratory
Dirección de correo verificada de arizona.edu
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Año
An efficient linear wavepacket tracking method for hypersonic boundary-layer stability prediction
OMF Browne, AP Haas, HF Fasel, C Brehm
Journal of Computational Physics 380, 243-268, 2019
392019
A time-spectral approximate Jacobian based linearized compressible Navier-Stokes solver for high-speed boundary-layer receptivity and stability
AP Haas, OMF Browne, HF Fasel, C Brehm
Journal of Computational Physics 405, 108978, 2020
252020
A nonlinear compressible flow disturbance formulation for adaptive mesh refinement wavepacket tracking in hypersonic boundary-layer flows
OMF Browne, AP Haas, HF Fasel, C Brehm
Computers & Fluids 240, 105395, 2022
242022
Linear Stability Investigation of Cross-Flow Instability for a Supersonic Swept Wing with a Biconvex Airfoil
AP Haas, C Hader, HF Fasel
AIAA Aviation 2021 Forum, 2848, 2021
182021
An efficient strategy for computing wave-packets in high-speed boundary layers
OM Browne, AP Haas, HF Fasel, C Brehm
47th AIAA Fluid Dynamics Conference, 3636, 2017
172017
A nonlinear wavepacket tracking method for hypersonic boundary-layer flows on irregular domains
OM Browne, AP Haas, HF Fasel, C Brehm
AIAA Aviation 2020 Forum, 2985, 2020
122020
A numerical Jacobian stability-solver based on the linearized compressible Navier–Stokes equations
AP Haas, OMF Browne, HF Fasel, C Brehm
AIAA Conference, Denver, CO, 4520, 2017
122017
A Numerical Jacobian Based Linearized Compressible Navier-Stokes Solver For Hypersonic Boundary-Layer Stability
AP Haas, OM Browne, HF Fasel, C Brehm
47th AIAA Fluid Dynamics Conference, 4520, 2017
92017
Direct numerical simulations of the nonlinear boundary layer transition regime on a blunt swept flat plate at Mach 6
M Leinemann, AP Haas, C Hader, HF Fasel
AIAA Paper 3557, 2023, 2023
52023
Numerical Investigations of Receptivity, Stability and Transition for High-Speed Boundary Layers
AP Haas
The University of Arizona, 2022
42022
Effects of Small Leading-Edge Bluntness on High-Speed Boundary-Layer Instabilities on Flat Plates
AP Haas, C Hader, HF Fasel
AIAA journal 62 (1), 162-174, 2024
32024
Numerical Investigations of Hypersonic Boundary-Layer Stability for a Blunt Flat Delta Wing
A Hartman, HF Fasel, S Wernz, AP Haas, C Hader
AIAA AVIATION 2023 Forum, 3443, 2023
32023
Machine-Learning-Based Transition Prediction for Hypersonic Boundary Layers with Crossflow
B Barraza, A Gross, AP Haas, C Hader, HF Fasel
AIAA SCITECH 2023 Forum, 2307, 2023
32023
Hypersonic heat transfer
A Haas
MS Thesis, School of Engineering, Aerospace, 2009
32009
Using Linear-Stability Theory to Build Transition Models
AP Haas, DM Israel
AIAA AVIATION 2023 Forum, 3571, 2023
22023
Machine-Learning-Based Amplification Factor Transport Equation for Hypersonic Boundary-Layers
B Barraza, A Gross, AP Haas, C Hader, H Fasel
AIAA AVIATION 2022 Forum, 3681, 2022
22022
Numerical Investigation of Cross-Flow Instability for a Supersonic Swept Wing with a Biconvex Airfoil
AP Haas, C Hader, HF Fasel
AIAA SCITECH 2022 Forum, 1074, 2022
22022
Heat transfer effects and topology of the viscous interaction induced by surface protuberances in hypersonic flow
A Haas, D MacManus, D Estruch-Samper
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2012
22012
ASSESSMENT AND VALIDATION OF INTERMITTENCY TRANSPORT EQUATIONS FOR MODELING HYPERSONIC TRANSITION WITH COOLFluiD AND CFD+
A Haas
Technical report, von Karman Institute for Fluid Dynamics Project report VKI …, 2010
22010
Shaken not stirred: Modeling the entire mixing process (Rev. 1)[Slides]
AP Haas, DM Israel
Los Alamos National Laboratory (LANL), Los Alamos, NM (United States), 2024
2024
El sistema no puede realizar la operación en estos momentos. Inténtalo de nuevo más tarde.
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