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Page 1: Aerospace Computing Lab - Homeaero-comlab.stanford.edu/Papers/presentation...aiaa... · Created Date: 7/17/2017 4:11:48 PM
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Aerodynamic Shape Optimization for Supersonic Aircraftaero-comlab.stanford.edu/jmartins/doc/AIAA_2002-2838-JR.pdf · AIAA 2002-2838 Aerodynamic Shape Optimization for Supersonic Aircraft

AIAA 2002-0949 Time-Dependent Aeroelastic Simulation of ...aero-comlab.stanford.edu/vdweide/Edwin.AIAA-2002-0949-Z.pdf · AIAA-2002-0949 1 American Institute of Aeronautics and Astronautics

Re-Engineering the Design Process Through Computationaero-comlab.stanford.edu/Papers/AIAA-2412-887.pdf · Re-Engineering the Design Process Through Computation Antony Jameson* Princeton

AIAA 2003Œ3531 - Stanford Universityaero-comlab.stanford.edu/Papers/shankaran.aiaa.03-3501.pdf · AIAA 2003Œ3531 Numerical Analysis and Design of Upwind Sails Sriram and Antony

AutomatedOff-Body CartesianMeshAdaptionfor …aero-comlab.stanford.edu/Papers/AIAA-2011-1269-888.pdfAutomatedOff-Body CartesianMeshAdaptionfor Rotorcraft Simulations SeanJ.Kamkar∗

Aerodynamic Design Studies of Conventional and ...aero-comlab.stanford.edu/Papers/AIAA-2006-3455-957.pdf · Aerodynamic Design Studies of Conventional & ... CP Coefficient of Pressure

AIAA 2004–4480 - Stanford Universityaero-comlab.stanford.edu/Papers/alonso.aiaa.04-4480.pdf · Juan J. Alonso∗, Patrick LeGresley †, Edwin van der Weide ‡ Stanford University

(c)2001 American Institute of Aeronautics & Astronautics ...aero-comlab.stanford.edu/Papers/aiaa-01-2530-326.pdf(c)2001 American Institute of Aeronautics & Astronautics or Published

Advanced Algorithms for Design and Optimization of Quiet …aero-comlab.stanford.edu/Papers/juanjo.aiaa02-0144.pdf · AIAA 2002–0144 Advanced Algorithms for Design and Optimization

Shock detection and capturing methods for high order ...aero-comlab.stanford.edu/Papers/AIAA-Paper_2014-2688.pdf32nd AIAA Applied Aerodynamics Conference High-order Discontinuous Galerkin

AIAA Applied Aerodynamics Conference, 16-20 June 2014 ...aero-comlab.stanford.edu/jleffell/publications/leffell.aiaa.14-3258.pdf · AIAA-2014-3258 32nd AIAA Applied Aerodynamics Conference,

Aerospace Computing Lab - Homeaero-comlab.stanford.edu/jxyao/aiaa00_reno.pdf · 2019. 6. 23. · -4/ '(k e ( * ) '(k < ! " $# &% ')(¯

44th AIAA Aerospace Sciences Meeting and Exhibit, …aero-comlab.stanford.edu/arathi/TSComputeTimep.pdfArathi K. Gopinath⁄, and Antony Jameson y ... the periodic nature of the problem,

p-Multigrid Spectral Difference Method For Viscous ...aero-comlab.stanford.edu/Papers/AIAA-2009-950-903.pdf§Professor, Department of Aerospace Engineering, Iowa State University,

AIAA 2001–0922 - Stanford Universityaero-comlab.stanford.edu/Papers/chung.aiaa.01-0922.pdf · AIAA 2001–0922 Using Gradients to Construct Response Surface Models for High-Dimensional

Advances in Bringing High-Order Methods to Practical ...aero-comlab.stanford.edu/Papers/AIAA-2011-3226-243.pdfApplications in Computational Fluid Dynamics Antony Jameson Aeronautics

Aerospace Computing Lab - Homeaero-comlab.stanford.edu/Papers/jameson_gente_motori...' Il dottor Wolfgang Schmidt, co. autore dello studio per GENTE MOTORI, nato nel 1942 a Dui- sburg,

Aerodynamic shape optimization of complex aircraft ...aero-comlab.stanford.edu/Papers/AIAA-1996-94-343.pdfAerodynamic Shape Optimization of Complex Aircraft Configurations via an Adjoint

Solution of steady three-dimensional compressible Euler and Navier …aero-comlab.stanford.edu/Papers/AIAA-1988-619-137.pdf · 2019-06-23 · AIAA-88-0619 Solution of Steady Three-Dimensional

Computational Sports Aerodynamics of a Moving Sphere ...aero-comlab.stanford.edu/Papers/AIAA-2011-3668-697.pdf · Computational Sports Aerodynamics of a Moving Sphere: Simulating

AIAA 2003–3698 - Aerospace Computing Lab - Homeaero-comlab.stanford.edu/Papers/reynolds.aiaa.03-3698.pdfFig. 1 The PW6000 aircraft gas turbine engine. Engine Component Simulation

Accelerating three-dimensional Navier-Stokes calculationsaero-comlab.stanford.edu/Papers/AIAA-1997-1953-176.pdfsolution of the Navier-Stokes equations remains one rithm must be based

1998/1999 AIAA Foundation Graduate Team Aircraft Design ...aero-comlab.stanford.edu/plegresl/presentations/wac2000.pdf · Cardinal Design Project Stanford University 1998/1999 AIAA

Mesh refinement and modelling errors ... - Stanford Universityaero-comlab.stanford.edu/Papers/AIAA-1996-2050-231.pdfdependent empirical observation such as experimen-tal data at high

Reduction of the Adjoint Gradient Formula for …aero-comlab.stanford.edu/Papers/kim_jameson_2003.pdf · AIAA JOURNAL Vol.41,No. 11, November2003 Reduction of the Adjoint Gradient

AIAA 2004–0763 - Stanford Universityaero-comlab.stanford.edu/Papers/hosseini.aiaa.04-0763.pdf · 2019. 6. 23. · AIAA 2004–0763 Practical Implementation and Improvement of Preconditioning

51st AIAA Aerospace Sciences Meeting including the New ...aero-comlab.stanford.edu/jleffell/publications/leffell.aiaa.13-0637.pdf · 51st AIAA Aerospace Sciences Meeting including

AIAA 2002–1483 - Aerospace Computing Labaero-comlab.stanford.edu/jmartins/doc/denver2002.pdfAIAA 2002–1483 High-Fidelity Aero-Structural Design Optimization of a Supersonic Business

AIAA 2004–1758 - Stanford Universityaero-comlab.stanford.edu/Papers/choi.aiaa.04-1758.pdf · AIAA 2004–1758 Design of a Low-Boom Supersonic Business Jet Using Evolutionary Algorithms

Dynamic Mesh Deformation for Adaptive Grid Resolution ...aero-comlab.stanford.edu/Papers/AIAA-2011-196-221.pdf · Dynamic Mesh Deformation for Adaptive Grid Refinement with Staggered

43rd AIAA Aerospace Sciences Meeting and Exhibit, January ...aero-comlab.stanford.edu/Papers/gopinath.aiaa.05-1220.pdf · 43rd AIAA Aerospace Sciences Meeting and Exhibit, January

Aerospace Computing Lab - Homeaero-comlab.stanford.edu/Papers/jameson_bangalore_1994-2.pdf · Created Date: 1/26/2008 11:46:52 AM

Studies of Wings Supporting Non-unique Solutions in Transonic …aero-comlab.stanford.edu/Papers/AIAA-Paper_2014-2928.pdf · 2019-06-23 · ∗Flight Sciences Department, Honda Aircraft

AIAA 2003–3429 - Stanford Universityaero-comlab.stanford.edu/Papers/alonso.aiaa.03-3429.pdf · 2019. 6. 23. · AIAA 2003–3429 High-Fidelity Aero-Structural Design Using a Parametric

Design of Adjoint Based Laws for Wing Flutter Controlaero-comlab.stanford.edu/Papers/AIAA-2009-148-555.pdf · 2019. 6. 23. · 47th AIAA Aerospace Sciences Meeting and Exhibit, January,