CEASIOM

Conceptual Aircraft Design

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Scientific publications related to CEASIOM

 

AIAA Atmospheric Flight Mechanics Conference, Toronto, 2 - 5 August 2010


A special session called "Outcomes from the EU SimSAC project: Simulating Stability and Control" was dedicated to CEASIOM during this conference.

The program of the session was:
  • "Modeling & Simulating Aircraft Stability & Control – SimSAC Project", A. W. Rizzi
  • "Flight Manoeuvre Validation of Data Tables Generated Using an Aerodynamic Model Hierarchy", K. J. Badcock; M. Ghoreyshi; A. Da Ronch; D. Vallespin; J. Vos; S. Hitzel
  • "From Geometry to CFD Grids - An Automated Approach for Conceptual Design", M. M. Tomac; D. Eller; A. Rizzi; J. Oppelstrup
  • "NeoCASS: an integrated tool for structural sizing, aeroelastic analysis and MDO at conceptual design level", S. Ricci; L. Cavagna; L. Travaglini
  • "Stability analysis in conceptual design using SDSA tool", T. Goetzendorf-Grabowski; D. Mieszalski; E. Marcinkiewicz
  • "Comparison of Conventional and Z-wing VLJ Designs using CEASIOM", T. S. Richardson; C. McFarlane; C. Beaverstock; A. Isikveren
  • "Benchmarking the prediction of dynamic derivatives: Wind tunnel tests, validation, acceleration methods", B. Mialon; A. Khrabov; S. Ricci; P. Eliasson; A. Huebner; R. Larsson
  • "Virtual Aircraft Design & Control of TransCruiser – a Canard Configuration", A. W. Rizzi; P. Eliasson; C. McFarlane; T. Goetzendorf-Grabowski; J. Vos

Other publications directly related to CEASIOM:

 

  • M. Ghoreyshi ,K. J. Badcock and M. A. Woodgate: “Integration of Multi-Fidelity Methods for Generating an Aerodynamic Model for Flight Simulation”, 46th AIAA Aerospace Sciences Meeting, January 2008
  • L. Cavagna, L. Riccobene, S. Ricci, A. Berard, A. Rizzi: “A Fast MDO tool for Aeroelastic Optimization in Aircraft Conceptual Design”, 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference in Canada, September 2008
  • A. Rizzi, R. von Kaenel: “CEASIOM: Simulating Stability & Control with CFD/CSM in Aircraft Conceptual Design”, ICAS 2008, Anchorage, Alaska, USA, September 14-19,2008
  • A. Berard, A. Rizzi, A.T. Isikveren L. Cavagna, S. Ricci, L. Riccobene: “Development and Validation of a Next-Generation Conceptual Aero-Structural Sizing Suite”, ICAS 2008, September 2008, Anchorage, Alaska
  • L.Cavagna, P.Masarati, S.Ricci and P.Mantegazza: “Development and Validation of an Investigation Tool for Nonlinear Aeroelastic Analysis”, 26. Intenational congress of the aeronautical sciences : ICAS 2008. Anchorage, Alaska. September 14-19, 2008., 2008-9.6.3, p. 1-10
  • T. Goetzendorf-Grabowski : “Flight Dynamic Analysis of an Aircraft within the Conceptual Stage of the Aircraft Design”, RRDPAE conference in Brno, Oct 2008.
  • P. Eliasson, P. Weinerfelt, J. Nordström: “Application of a line-implicit scheme on stretched unstructured grids”, 47th AIAA Aerospace Sciences Meeting, January 2009.
  • M. Ghoreyshi, K. J. Badcock, M. A. Woodgate: “Accelerating the Numerical Generation of Aerodynamic Models for Flight Simulation”, 47th AIAA Aerospace Sciences Meeting, January 2009.
  • A.R. Huebner, A. Bergmann, T. Loeser: “Experimental and numerical investigations of unsteady force and pressure distributions of moving transport aircraft configuration”, 47th AIAA Aerospace Sciences Meeting, January 2009.
  • C. S. Beaverstock, A. Maheri, T. S. Richardson, M. H. Lowenberg and A. T. Isikveren: “Methods for Conceptual Flight Control System Design”, 47th AIAA Aerospace Sciences Meeting, January 2009.
  • L. Cavagna, S. Ricci and L. Riccobene: “Application of Adaptive Camber Mechanism to Morphing Wings”, RTO-NATA-AVT 168 Symposium on Morphing Aircraft, Evora, 20-24 April, 2009.
  • P. Molitor, M. Tomax and A. Rizzi: “X-31 Engineering Predictions for S&C”, RTO-NATA-AVT 168 Symposium on Morphing Aircraft, Evora, 20-24 April, 2009.
  • L. Cavagna , L. Riccobene , S. Ricci, A. Berard , A. Rizzi: “A Fast Tool for Structural Sizing, Aeroelastic Analysis and Optimization in Aircraft Conceptual Design”, 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization, 10-12 September 2008, Victoria, British Columbia Canada
  • A. Scotti, L. Cavagna and S. Ricci: “Conceptual Design of a three surface aircraft including aeroelastic constraints”, International Forum of Aeroelasticity and Structural Dynamics, Seattle, June 21-24, 2009.
  • L. Cavagna and S. Ricci : “Bringing Aeroelastic Analysis in the Conceptual Design of Future Aircraft”, International Forum of Aeroelasticity and Structural Dynamics, Seattle, June 21-24, 2009.
  • L. Cavagna and S. Ricci: “NeoCASS: a tool for Aeroelastic Optimization at Aircraft Conceptual Design Level”, International Forum of Aeroelasticity and Structural Dynamics, Seattle, June 21-24, 2009.
  • T. Goetzendorf-Grabowski et al.: “Coupling Adaptive-Fidelity CFD with S&C Analysis to Predict Flying Qualities”, 27th AIAA Applied Aerodynamics Conference, June 2009.
  • B. Mialon et al.: “European Benchmark on Numerical Prediction of Stability and Control derivatives”, 27th AIAA Applied Aerodynamics Conference, June 2009.
  • M. Ghoreyshi et al.: “Aerodynamic Modelling for Flight Dynamics Analysis of Conceptual Aircraft Designs”, 27th AIAA Applied Aerodynamics Conference, San Antonio, TX June 2009.
  • A. Rizzi et al.: “Creating Aero-Databases by Adaptive-Fidelity CFD Coupled with S&C Analysis”, CEAS Conference in Manchester, October 2009.
  • L. Cavagna et al.: “Conceptual Design of Unconventional Aircraft: Application to Tilt Rotor Aeroelastic Sizing“, CEAS Conference in Manchester, October 2009.
  • R. Larsson et al.: “Industry Perspectives on SimSAC Tools and Their use in Designing New Concepts”, CEAS Conference in Manchester, October 2009.
  • A. Khrabrov et al.: “Non-Symmetrical General Aviation Aircraft and Flight Control Law Design using CEASIOM Software”, AIAA Aerospace Sciences Meeting, Orlando in January 2010.
  • M. Tomac et al.: “Creation of Aerodynamic Data base for the X31”, AIAA Aerospace Sciences Meeting, Orlando in January 2010.
  • A. DaRonch, et al.: "Linear Frequency Domain and Harmonic Balance Predictions of Dynamic Derivatives", 28th AIAA Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun-1 Jul 2010.
  • A. Rizzi: “Modeling & Simulating Aircraft Stability & Control – SimSAC Project”, 28th AIAA Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun-1 Jul 2010.
  • M. Ghoreyshi, D. Vallespin, K.J. Badcock, A. Da Ronch, J. Vos, S. Hitzel: “Flight Manoeuvre Validation of Data Tables Generated Using an Aerodynamic Model Hierarchy”, 28th AIAA Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun-1 Jul 2010.
  • J. Oppelstrup, D. Eller, M. Tomax, A. Rizzi: “From Geometry to CFD Grids – An Automated Approach for Conceptual Design”, 28th AIAA Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun-1 Jul 2010.
  • L. Cavagna, S. Ricci, L. Travaglini: “NeoCASS: an Integrated Tool for Structural Sizing, Aeroelastic Analysis and MDO at Conceptual Design Level”, 28th AIAA Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun-1 Jul 2010.
  • T. Goetzendorf-Grabowski, D. Mieszalski, E. Marcinkiewiciz: “Stability Analysis in Conceptual Design using the SDSA Tool”, 28th AIAA Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun-1 Jul 2010.
  • C. McFarlane, T. Richardson, C. Beaverstock: “Comparison of Conventional and Z-wing VLJ Designs using CEASION”, 28th AIAA Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun-1 Jul 2010.
  • B. Mialon, A. Khrabov S. Ricci, P. Eliasson, A. Huebner, R. Larsson: “Benchmarking the Prediction of Dynamic Derivatives: Wind Tunnel Tests, Validation, Acceleration Methods”, 28th AIAA Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun-1 Jul 2010.
  • A. Rizzi, P. Eliasson, C. McFarlane, T. Goetzendorf-Grabowski, J.B. Vos: “Virtual Aircraft Design & Control of TransCruiser – a Canard Configuration”, 28th AIAA Applied Aerodynamics Conference, Chicago, Illinois, 28 Jun-1 Jul 2010.
  • M. Ghoreyshi, K. Badcock, M. Woodgate : “Accelerating the Numerical Generation of Aerodynamic Models for Flight Simulation”, Journal of Aircraft 2009 0021-8669 vol.46 no.3 (972-980) DOI: 10.2514/1.39626