[1]

M Aftomis, M Berger, and G Adomavicius. A parallel multilevel method for adaptively refined cartesian grids with embedded boundaries. Number AIAA-2008-0808, Reno, NV, Jan. 2008. American Institute of Aeronautics and Astronautics.

[2]

Robert T. Biedron, Jan-Renee Carlson, Joseph M. Derlaga, Peter A. Gnoffo, Dana P. Hammond, William T. Jones, Bil Kleb, Elizabeth M. Lee-Rausch, Eric J. Nielsen, Michael A. Park, Christopher L. Rumsey, James L. Thomas, and William A. Wood. FUN3D Manual: 12.7, May 2015.

[3]

Dean E. Bryson, Robert Haimes, and John Dannenhoffer. Toward the realization of a highly integrated, multidisciplinary, multifidelity design environment. In AIAA Scitech 2019 Forum.

[4]

William Case. MYSTRAN General Purpose Finite Element Structural Analysis Computer Program (Linux Version 6.35) [Software Manual], Nov. 2011. Available from http://www.MYSTRAN.com.

[5]

John Dannenhoffer and Nitin Bhagat. Towards modeling for design: Using real-time collaborative environment in caps. In AIAA Scitech 2022 Forum.

[6]

John Dannenhoffer and Robert Haimes. Conservative fitting for multi-disciplinary analysis. In 52nd Aerospace Sciences Meeting, number 2014-0294. American Institute of Aeronautics and Astronautics, Jan. 2014.

[7]

John Dannenhoffer. Opencsm: An open-source constructive solid modeler for mdao. In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, number 2013-0701. American Institute of Aeronautics and Astronautics, Jan. 2013.

[8]

Dassault Systèmes. http://www.3ds.com/products-services/simulia/products/abaqus/. Accessed: May 2016.

[9]

Julia Docampo-Sanchez and Robert Haimes. Towards fully regular quad mesh generation. In AIAA Scitech 2019 Forum.

[10]

Mark Drela and Harold Youngren. AVL (Athena Vortex Lattice) 3.30 User Primer, Aug. 2010. Available from http://web.mit.edu/drela/Public/web/avl/.

[11]

Mark Drela, Marshall Galbraith, Robert Haimes, Steven R. Allmaras, and David Darmofal. Hybrid shell model for aeroelastic modeling. In AIAA Scitech 2019 Forum.

[12]

Ryan J. Durscher and Dennis Reedy. pycaps: A python interface to the computational aircraft prototype syntheses. In AIAA Scitech 2019 Forum.

[13]

Robert Haimes and John Dannenhoffer. The engineering sketch pad: A solid-modeling, feature-based, web-enabled system for building parametric geometry. In 21st AIAA Computational Fluid Dynamics Conference, number 2013-3073. American Institute of Aeronautics and Astronautics, Jun. 2013.

[14]

Robert Haimes and Mark Drela. On the construction of aircraft conceptual geometry for high-fidelity analysis and design. In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, number 2012-0683. American Institute of Aeronautics and Astronautics, Jan. 2012.

[15]

Chritopher M. Heath and Justin S. Gray. OpenMDAO: Framework for Flexible Multidisciplinary Design, Analysis and Optimization Methods. In 8th AIAA Multidisciplinary Design Optimization Specialist Conference (MDO), pages 1–13, Honolulu, Hawaii, 2012.

[16]

Steve L. Karman and Nicholas J. Wyman. Automatic unstructured mesh generation with geometry attribution. In AIAA Scitech 2019 Forum.

[17]

Raymond M. Kolonay. A physics-based distributed collaborative design process for military aerospace vehicle development and technology assessment. International Journal of Agile Systems and Management, 7(3-4):242–260, 2014.

[18]

David L. Marcum and Nigel P. Weatherill. Unstructured grid generation using iterative point insertion and local reconnection. AIAA Journal, 33(9):1619–1625, Sep. 1995.

[19]

David L Marcum. Unstructured grid generation using automatic point insertion and local reconnection. The Handbook of Grid Generation, pages 18–1, 1998.

[20]

W. H. Mason. FRICTION - Skin Friction and Form Drag Program, Jan. 2006. Available from http://www.dept.aoe.vt.edu/ mason/Mason_f/MRsoft.html.

[21]

L. A. McCullers. AWAVE: User's Guide for the Revised Wave Drag Analysis Program, Apr. 1992.

[22]

F. Palacios, M. R. Colonno, A. C. Aranake, A. Campos, S. R. Copeland, T. D. Economon, A. K. Lonkar, T. W. Lukaczyk, T. W. R. Taylor, and J. J. Alonso. Stanford university unstructured (su2): An open-source integrated computational environment for multi-physics simulation and design. In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, number 2013-0287. American Institute of Aeronautics and Astronautics, Jan. 2013.

[23]

F. Palacios, T. D. Economon, A. C. Aranake, S. R. Copeland, A. K. Lonkar, T. W. Lukaczyk, D. E. Manosalvas, K. R. Naik, A. S. Padron, B. Tracey, A. Variyar, and J. J. Alonso. Stanford university unstructured (su2): Open-source analysis and design technology for turbulent flows. In 52nd Aerospace Sciences Meeting, number 2014-0243. American Institute of Aeronautics and Astronautics, Jan. 2014.

[24]

Phoenix Integration. http://www.phoenix-int.com/. Accessed: May 2016.

[25]

Michael Reymond and Mark Miller. MSC NASTRAN Quick Reference Guide Version 68, 1996.

[26]

Hang Si. Tetgen, a delaunay-based quality tetrahedral mesh generator. ACM Trans. Math. Softw., 41(2):11:1–11:36, Feb. 2015.