CAPS
Analysis Interface Module (AIM)
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Bibliography
[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]

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.

[4]

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

[5]

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/.

[6]

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

[7]

Mark Drela. Xfoil: An analysis and design system for low reynolds number airfoils. In Thomas J. Mueller, editor, Low Reynolds Number Aerodynamics: Proceedings of the Conference Notre Dame, Indiana, USA, 5–7 June 1989, pages 1–12, Berlin, Heidelberg, 1989. Springer Berlin Heidelberg.

[8]

Mark Drela. A user’s guide to mses 3.05, Jul 2017.

[9]

Altair flightstream.

[10]

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.

[11]

David Kinney. Aero-thermodynamics for conceptual design. Number AIAA-2004-31, Reno, NV, Jan. 2004. 42nd AIAA Aerospace Sciences Meeting and Exhibit.

[12]

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.

[13]

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

[14]

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.

[15]

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

[16]

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.

[17]

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.

[18]

Micheal Park. NASA refine.

[19]

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

[20]

Christopher Rosema, Joshua Doyle, and William B. Blake. MISSILE DATA COMPENDIUM (DATCOM) User Manual – 2014 Revision [Software Manual], afrl-rq-wp-tr-2014-0281 edition, Dec. 2014.

[21]

Toolkit for the analysis of composite structures (TACS).

[22]

Zona Technology. Zona technology ZAERO.