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AAA in Publications

AAA is widely used throughout the world by industry and academia. From conceptual to preliminary design, from research to analysis, AAA gives users a versatile aeronautical tool to address unique needs. Presented below are the partial listings of AAA used in books and papers published over the last decade.

Books

  • Martin Kozek, Alexander Schirrer (Editors), Modeling and Control for a Blended Wing Body Aircraft, Springer Verlag, 2014.
  • Antonio Filippone, Advanced Aircraft Flight Performance, Cambridge Aerospace Series, Cambridge University Press, 2012
  • Mark Tischler, Robert Remple, Aircraft and Rotorcraft System Identification (AIAA Education Series), AIAA, 2006
  • Bernd Chudoba, Stability and Control of Conventional and Unconventional Aircraft Configurations, Books On Demand, 2002.

Papers

  • M. Vedantam, S. Keshmiri, G.Garcia, W. Huang, “Fixed Wing Aircraft Perching Fixed Wing Aircraft Perching”, presented at the 55th AIAA Aerospace Sciences Meeting, AIAA Science and Technology Forum and Exposition, January 9-13, 2017, Grapevine, Texas.
  • Hugh C. Briggs, “A Survey of Integrated Tools for Air Vehicle Design, Part II”, AIAA 2015-0803, AIAA SciTech 2015, 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Kissimmee, Florida, January 5-9, 2015.
  • Hugh C. Briggs, “A Survey of Integrated Tools for Air Vehicle Design, Part I”, AIAA 2015-0802, AIAA SciTech 2015, 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Kissimmee, Florida, January 5-9, 2015.
  • Zhang, M., Cristofaro, M., Wang, Yongzhi, Da Ronch, A. and Rizzi, A. ” Investigating the Piaggio Avanti design using CEASIOM”, 29th Congress of the International Council of the Aeronautical Sciences (ICAS 2014), Russian Federation, RU, 07 – 12 September 2014. Internatioanl Council Aeronautical Sciences (ICAS) 11 pp.
  • Daniel M. Kennedy, Alex E. Sizemore, Nathan A. Smith, Luiz F. Toledo. “Dynamic Analysis of the Meridian Unmanned Aerial Vehicle”, AIAA Atmospheric Flight Mechanics Conference, AIAA 2014-0191, January 2014.
  • Oliver, R. , The Hexplane: A Scalable Air Vehicle Concept for Breakthrough Performance in Speed and VTOL, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA 2013-1089, January 2013
  • G. Fuentes, C. Agudelo, L. Palacio, “Initial Weight Analysis of a Next Generation Light Attack/Armed Reconnaissance Aircraft (LAAR)”, AIAA 2013-1086, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Grapevine, Texas, 2013.
  • M. Sharma, T.R. Reddy, C.I. Priyadarsini, Flow Analysis, over an F-16 Aircraft Using Computational Fluid Dynamics, International Journal of Emerging Technology and Advanced Engineering, Volume 3, Issue,5, 2013
  • G. Garcia, S. Keshmiri, “Adaptive and Resilient Flight Control System for a Small Unmanned Aerial System”, International Journal of Aerospace Engineering, Volume 2013, Article 289357, 2013.
  • Thompson, E. C., McCafferty, J. P., & Sellers, J. B. Advanced Aircraft Analysis of the Yak-54 40%., Guidance, Navigation, and Control and Co-located Conferences, 2013
  • O. Daskiran, M.S. Kavsaoglu, Flight Dynamics Analysis And Control Of Transport Aircraft Subject To Failure, Progress in Flight Dynamics, GNC, and Avionics 6 (2013) 347-362
  • Seitz, “Advanced methods for propulsion system integration in aircraft conceptual design.” PhD diss., Dissertation, Institut for Luft-und Raumfahrt, Technische University Munchen. Munich, 2012.
  • Amanda Lampton, John Valasek, Prediction of icing effects on the lateral/directional stability and control of light airplanes, Aerospace Science and Technology, Volume 23, Issue 1, December 2012, Pages 305-311
  • J. van Dommelen, R. Vos, A Conceptual Design And Analysis Tool For Blended Wing Body Aircraft, 28th Congress of the International Council of the Aeronautical Sciences, 23 – 28 September 2012, Brisbane, Australia, Paper ICAS 2012-1.7.2
  • C. Liersch, M. Herpperle, “A Distributed Toolbox for Multidisciplinary Preliminary Aircraft Design”, CEAS Aeronautical Journal, Volume 2, Issue 1-4, pp 57-68, December 2011.
  • M. Zhang, “Application and Development of the CEASIOM-SUMO-EDGE Suite for Rapid AeroData Assessment of Aircraft Flying Qualities.” 2011.
  • R. Lykins, R. Riley, G. Garcia, S. Keshmiri, “Modal Analysis of 1/3-Scale Yak-54 Aircraft Through Simulation and Flight Testing”, AIAA 2011-6443, AIAA Atmospheric Flight Mechanics Conference, Portland, Oregon, August, 2011.
  • R. Hale, E. Arnold, M. Ewing, W. Liu, Method for Design and Analysis of Externally Mounted Antenna Fairings in Support of Cryospheric Surveying, 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, AIAA-2011-1714
  • B.C. Sweeten, “CFD Analysis of UAVs using VORSTAB, FLUENT, and Advanced Aircraft Analysis Software.” PhD diss., University of Kansas, 2010.
  • N. Anton, R.M. Botez, D. Popescu, “New Methodology and Code for Hawker 800XP Aircraft Stability Derivatives Calculations from Geometrical Data.” The Aeronautical Journal 114, no. 1156, 2010.
  • D. Royer, S. Keshmiri, Modeling and Sensitivity Analysis of the Meridian Unmanned Aircraft, AIAA InfoTech Aerospace 2010, AIAA 2010-3468
  • B.C. Sweeten, D. Royer, S. Keshmiri. “The Meridian UAV Flight Performance Analysis Using Analytical and Experimental Data.”AIAA Infotech@ Aerospace Conf., Seattle, WA, AIAA Paper, vol. 1899. 2009.
  • Antonio Filippone, Comprehensive analysis of transport aircraft flight performance, Progress in Aerospace Sciences, Volume 44, Issue 3, April 2008, Pages 192-236
  • L. E. Casas, J. M. Hall, S. A. Montgomery, H. G. Patel, S. S. Samra, J. Si Tou, O. Quijano, Nikos J. Mourtos, and P. P. Papadopoulos. “Preliminary Design and CFD Analysis of a Fire Surveillance Unmanned Aerial Vehicle” Thermal-Fluids Analysis Workshop, TFAWS-08-1034.. Aug. 2008.
  • F. Caliskan, Neural Network Based Icing Identification and Fault Tolerant Control of a 340 Aircraft, World Academy of Science, Engineering and Technology, vol. 4, 2007-04-27
  • U. Ozdemir, E.M. Jafarov, M.S. Kavsaoglu, Calculation of the longitudinal stability derivatives of a transport aircraft and analysis of longitudinal modes, ACMOS’07 Proceedings of the 9th WSEAS international conference on Automatic control, modeling and simulation, 2007, World Scientific and Engineering Academy and Society (WSEAS)
  • T. Melin, A.T. Isikveren, A. Rizzi, C. Stamblewski, H.V. Anders, “How Industry Concepts of Concurrent Engineering Enhance Aircraft Design Education.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 221, no. 2, 175-192. 2007.
  • W. Donovan, “CReSIS UAV Critical Design Review: the Meridian.” CReSIS-TR-123 (2007).
  • S.S. Sarakinos, I.M. Valakos, “A Software Tool for Generic Parameterized Aircraft Design”, Advances in Engineering Software, Volume 38, Issue 1, January 2007.
  • Ro, K., Flight dynamic investigations of flying wing with winglet configured unmanned aerial vehicle. In Defense and Security Symposium (pp. 62280L-62280L). International Society for Optics and Photonics. Proc. SPIE 6228, Modeling and Simulation for Military Applications, April 2006
  • W. Park, “A Study on the Parameter Estimation of DURUMI-II for the Fixed Right Elevator Using Flight Test Data”, Journal of Mechanical Science and Technology, Volume 20, Issue 8, August 2006
  • R. Krashanitsa, G. Platanitis, B. Silin, S. Shkarayev, “Aerodynamics and Controls Design for Autonomous Micro Air Vehicles.” AIAA Atmospheric Flight Mechanics Conference and Exhibit, pp. 21-24, 2006.
  • Sugjoon Yoon, Ji-Young Kong, Kang-Su Kim, Suk-Kyung Lee, Moon-Sang Kim , Derivation of Flight Characteristics Data of Small Airplanes Using Design Software and Their Validation by Subjective Tests, Systems Modeling and Simulation: Theory and Applications, Lecture Notes in Computer Science Volume 3398, 2005, pp 450-457
  • Sadraey, M., Colgren, R. (2005, August). UAV flight simulation: credibility of linear decoupled vs. nonlinear coupled equations of motion. AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2005-6425
  • X. Huang, “A Prototype Computerized Synthesis Methodology for Generic Space Access Vehicle (SAV) Conceptual Design”, AIAA 2005-2539, AIAA 1st Space Exploration Conference: Continuing the Voyage of Discovery, Orlando, Florida, 2005.
  • G. Platanitis, S. Shkarayev, “Integration of an Autopilot for a Micro Air Vehicle”, Infotech@Aerospace, AIAA 2005-7066 (NASA Grant Report NNL04A462G), June 2005.
  • K.C. Markell, “Exergy Methods for the Generic Analysis and Optimization of Hypersonic Vehicle Concepts.” PhD diss., Virginia Polytechnic Institute and State University, 2005.
  • T. Foster, W.J. Bowman, “Dynamic Stability and Handling Qualities of Small Unmanned Aerial Vehicles.” 43rd AIAA Aerospace Sciences Meeting and Exhibit, pp. 10-13. 2005.
  • J. Henry, J. Blondeau, D. Pines, “Stability Analysis for UAVs with a Variable Aspect Ratio Wing.” AIAA 2005-2044, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Austin, Texas, April 2005.
  • Matthew A. Bennington and Kenneth D. Visser. “Aerial Refueling Implications for Commercial Aviation”, Journal of Aircraft, Vol. 42, No. 2 (2005), pp. 366-375.
  • Uygun, M., & Tuncer, I. H. (2004). Viscous flow solutions over CN-235 cargo aircraft. Journal of Aircraft, 41(4), 940-944.
  • V. Janardhan, D. Schmitz, S.N. Balakrishnan, Development and implementation of new nonlinear control concepts for a UA, The 23rd Digital Avionics Systems Conference, 2004. DASC 04. Volume 2
  • Winther, B. A. (2003). Analytical representation of aerodynamic forces in Laplace domain. Journal of Aircraft, 40(2), 395-399.
  • Cengizhan Bahar, Nafiz Alemdaroglu, Yusuf Ozyoruk, and Emre Temel. “Euler Solutions for a Medium-Range Cargo Aircraft”, Journal of Aircraft, Vol. 40, No. 2 (2003), pp. 393-395.
  • D. Verstraete, P. Hendrick, “Preliminary Design of an ACES TSTO Air Launch Vehicle.” AIAA Paper 6997 (2003): 2003.
  • D.L. Daggett, S.T. Brown, R.T. Kawai, “Ultra-Efficient Engine Diameter Study”. National Aeronautics and Space Administration, Glenn Research Center, 2003.
  • M. S. Hwang, W. J. Park, Y. C. Kim, H. B. Eun, W. J. Choi, YK SONG. “Lateral Stability Improvement of a Canard Airplane Using a Vertical Panel.”AIAA Atmospheric Flight Mechanics Conference and Exhibit, p. 4625. 2002.
  • LeGresley, P., Bathke, T., Carrion, A., Cornejo, J. et al., 1998/1999 AIAA Foundation Graduate Team Aircraft Design Competition: Super STOL Carrier On-board Delivery Aircraft, SAE Technical Paper 2000-01-5535, 2000
  • D. Scholz, J. Thorbeck, Computer Based Training In Aircraft Design Education, ICAS2000 Congress, International Council of the Aeronautical Sciences , 1.7.3, 2000
  • D. Scholz, “Computer Aided Engineering for the Design of Flight Control and Hydraulic Systems”, SAE 961327, Journal of Aerospace, Vol. 105, Sec. 1, pp. 203-212, 1997.
  • J. Valasek, An Eclectic Approach to Undergraduate Flight Dynamics, Stability, and Control Education, AIAA Atmospheric Flight Mechanics Conference, AIAA-96-3373-CP, 1996
  • D.S. Gerren, “Design, Analysis, and Control of a Large Transport Aircraft Utilizing Selective Engine Thrust as a Backup System for the Primary Flight Controls.” National Aeronautics and Space Administration, Dryden Flight Research Facility, 1995.