Design of a canard configured TransCruiser using CEASIOM

Progress in Aerospace Sciences

Volumn 47, Issue 8, 2011, Pages 695-705

  Rizzi, Arthur ^a   Eliasson, Peter ^b   Goetzendorf Grabowski, Tomasz ^c   Vos, Jan B ^d   Zhang, Mengmeng ^a   Richardson, Thomas S ^e  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

^b SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^c WARSAW UNIVERSITY OF TECHNOLOGY   (Poland)

^d PSE   (Switzerland)

^e UNIVERSITY OF BRISTOL   (United Kingdom)

Author keywords

Aerodynamics; Aircraft design; CFD; Flight control; Flight dynamics; Simulation

Indexed keywords

AERODYNAMICS; AEROELASTICITY; COMPUTATIONAL FLUID DYNAMICS; DEGREES OF FREEDOM (MECHANICS); ELECTRIC REACTORS; FLIGHT CONTROL SYSTEMS; FLIGHT DYNAMICS; FLIGHT SIMULATORS; SUPERSONIC AIRCRAFT; WIND TUNNELS;

AIRCRAFT DESIGN; CONVENTIONAL METHODS; FLIGHT CONTROL; MULTIDISCIPLINARY SOFTWARE; SIMULATION; SIMULATION AND ANALYSIS; SIX DEGREES OF FREEDOM; SOFTWARE ENVIRONMENTS;

COMPUTER AIDED DESIGN;

EID: 81155137799     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.paerosci.2011.08.011     Document Type: Review

References (11)

1. Rizzi A. Modeling & simulating aircraft stability & control: the SimSAC project. Special Session AIAA AFM conference, Toronto, 2010.
2. von Kaenel R, Rizzi A, Oppelstrup J, Goetzen T, Ghoreyshi M, Cavagna L, Bérard A. CEASIOM: simulating stability & control with CFD/CSM in aircraft conceptual design, Paper 061. In: 26th international congress of the aeronautical sciences, Anchorage, Alaska, September 2008.
3. Isikveren AT. Quasi-analytical modeling and optimization techniques for transport aircraft design. Report 2002-13. Doctoral dissertation, Royal Institute of Technology (KTH), Department of Aeronautics, Sweden, 2002.
4. Si H. On refinement of constrained Delaunay tetrahedralizations. In: Proceedings of the 15th international meshing roundtable, September 2006. Software available from 〈 http://tetgen.berlios.de 〉, July 2009.
5. Mialon B, Khrabov A, Ricci S, Eliasson P, Huebner A, Larsson R. Benchmarking the prediction of dynamic derivatives: Wind tunnel tests, validation, acceleration methods. Special session AIAA AFM conference, Toronto, 2010.
6. Eliasson P, Vos J, Da Ronch A, Zhang M, Rizzi A. Virtual aircraft design of TransCruiser computing break points in pitch moment curve. AIAA-2010-4366, 2010.
7. Lophaven SN, Nielsen HB, Sondergaard J. DACE, a Matlab Kriging Toolbox. Version 2.0, August 1, 2002. Technical report IMM-TR-2002-12. Technical University of Denmark.
8. Lophaven SN, Nielsen HB, Sondergaard J. Aspects of the Matlab Toolbox DACE. Technical report IMM-REP-2002-12. Technical University of Denmark.
9. Melin T. TORNADO a Vortex-Lattice MATLAB implementation for linear aerodynamic wing applications. Masters thesis. Sweden: Royal Institute of Technology (KTH), Department of Aeronautics; December 2000.
10. Eller D. Mesh generation using sumo and tetgen. KTH SimSAC report D2.3-5, 2009.
11. Puelles A. Further development and application of CEASIOM to the transonic cruiser design. Master thesis. Sweden: Royal Institute of Technology (KTH), Department of Aeronautics; February 2009.