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Volumn 1, Issue , 2010, Pages

An integrated computational/experimental approach to UCAV stability & control estimation: Overview of NATO RTO AVT-161

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; FLIGHT CONTROL SYSTEMS; FORECASTING; INTEGRATED CONTROL;

EID: 78649503223     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4392     Document Type: Conference Paper
Times cited : (69)

References (79)
  • 1
    • 3042831082 scopus 로고    scopus 로고
    • Historical review of uncommanded lateral-directional motions at transonic conditions
    • Chambers, J.R. and Hall, R.M., "Historical Review of Uncommanded Lateral-Directional Motions at Transonic Conditions," Journal of Aircraft, Vol. 41, No. 3, 2004, pp. 436-447.
    • (2004) Journal of Aircraft , vol.41 , Issue.3 , pp. 436-447
    • Chambers, J.R.1    Hall, R.M.2
  • 2
    • 22544475340 scopus 로고    scopus 로고
    • Accomplishments of the abrupt-wing-stall program
    • Hall, R.M., Woodson, S.H., and Chambers, J.R., "Accomplishments of the Abrupt-Wing-Stall Program," Journal of Aircraft, Vol. 42, No. 3, 2005, pp. 653-660.
    • (2005) Journal of Aircraft , vol.42 , Issue.3 , pp. 653-660
    • Hall, R.M.1    Woodson, S.H.2    Chambers, J.R.3
  • 6
    • 0242273162 scopus 로고    scopus 로고
    • Status of unsteady aerodynamic prediction for flutter of high-performance aircraft
    • Yurkovich, R., "Status of Unsteady Aerodynamic Prediction for Flutter of High-Performance Aircraft," Journal of Aircraft, Vol. 40, No. 5, 2003, pp. 832-842.
    • (2003) Journal of Aircraft , vol.40 , Issue.5 , pp. 832-842
    • Yurkovich, R.1
  • 7
    • 0030142199 scopus 로고    scopus 로고
    • Full scale wind tunnel studies of F/A-18 tail buffet
    • Meyn, L. A. and James, K. D., "Full Scale Wind Tunnel Studies of F/A-18 Tail Buffet," Journal of Aircraft, Vol. 33, No. 3, 1996, pp. 589-595.
    • (1996) Journal of Aircraft , vol.33 , Issue.3 , pp. 589-595
    • Meyn, L.A.1    James, K.D.2
  • 9
    • 84894356641 scopus 로고    scopus 로고
    • Automation of a navier-stokes S&C database generation for the harrier in ground effect
    • Jan.
    • Murman, S.M., Chaderjian, N.M., and Pandya, S.A., "Automation of a Navier-Stokes S&C database generation for the Harrier in Ground Effect," AIAA Paper 2002-259, Jan. 2002.
    • (2002) AIAA Paper 2002-259
    • Murman, S.M.1    Chaderjian, N.M.2    Pandya, S.A.3
  • 10
    • 78649514975 scopus 로고    scopus 로고
    • Progress toward generation of a navier-stokes database for a harrier in ground effect
    • Jan.
    • Chaderjian, N.M., Ahmad, J., Pandya, S., and Murman, S.M., "Progress Toward Generation of a Navier-Stokes Database for a Harrier in Ground Effect," AIAA Paper 2002-5966, Jan. 2002.
    • (2002) AIAA Paper 2002-5966
    • Chaderjian, N.M.1    Ahmad, J.2    Pandya, S.3    Murman, S.M.4
  • 12
    • 78649515732 scopus 로고    scopus 로고
    • Conclusions and recommendations
    • 24-23
    • Verhaagen, N. and Huang, X., "Conclusions and Recommendations," NATO RTO-TR-AVT-080, 2009, pp. 24-1 to 24-3.
    • (2009) NATO RTO-TR-AVT-080 , pp. 24-21
    • Verhaagen, N.1    Huang, X.2
  • 13
    • 78649507036 scopus 로고    scopus 로고
    • RTO/AVT high reynolds number detached eddy simulations for vortex breakdwon over a 70 degree delta wing
    • 15-18
    • Morton, S.A., "RTO/AVT High Reynolds Number Detached Eddy Simulations for Vortex Breakdwon Over a 70 Degree Delta Wing," NATO RTO-TR-AVT-080, 2009, pp. 15-1 to 15-18.
    • (2009) NATO RTO-TR-AVT-080 , pp. 15-11
    • Morton, S.A.1
  • 14
    • 85051724595 scopus 로고    scopus 로고
    • Unsteady euler and detached-eddy simulations of full-span ONERA 70° delta wing
    • 13-36
    • Görtz, S., "Unsteady Euler and Detached-Eddy Simulations of Full-Span ONERA 70° Delta Wing," NATO RTO-TR-AVT-080, 2009, pp. 13-1 to 13-36.
    • (2009) NATO RTO-TR-AVT-080 , pp. 13-11
    • Görtz, S.1
  • 15
    • 84878731724 scopus 로고    scopus 로고
    • Simulation of vortical flow over ONERA 70-degree delta wing
    • 18-12
    • Soemarwoto, B.I., and Boelens, O.J., "Simulation of Vortical Flow over ONERA 70-Degree Delta Wing," NATO RTO-TR-AVT-080, pp. 18-1 to 18-12.
    • NATO RTO-TR-AVT-080 , pp. 18-11
    • Soemarwoto, B.I.1    Boelens, O.J.2
  • 16
    • 33947577697 scopus 로고    scopus 로고
    • The second international vortex flow experiment (VFE-2): Objectives and first results
    • Hummel, D., "The Second International Vortex Flow Experiment (VFE-2): Objectives and First Results," J. Aerospace Engineering, Vol. 220, No. 6, 2006, pp. 559-568.
    • (2006) J. Aerospace Engineering , vol.220 , Issue.6 , pp. 559-568
    • Hummel, D.1
  • 17
    • 78149433075 scopus 로고    scopus 로고
    • Review of the second international vortex flow experiment (VFE-2)
    • Jan.
    • Hummel, D., "Review of the Second International Vortex Flow Experiment (VFE-2)," AIAA Paper 2008-0377, Jan. 2008.
    • (2008) AIAA Paper 2008-0377
    • Hummel, D.1
  • 18
    • 78649528016 scopus 로고    scopus 로고
    • Initial experiments and analysis of vortex flow on blunt edged delta wings
    • Jan.
    • Luckring, J.M., "Initial Experiments and Analysis of Vortex Flow on Blunt Edged Delta Wings," AIAA Paper 2008-0378, Jan. 2008.
    • (2008) AIAA Paper 2008-0378
    • Luckring, J.M.1
  • 19
    • 78149440356 scopus 로고    scopus 로고
    • PSP and PIV investigations on the VFE-2 configuration in sub- and transonic flow
    • Jan.
    • Konrath, R., Klein, Ch., and Schroeder, A., "PSP and PIV Investigations on the VFE-2 Configuration in Sub- and Transonic Flow," AIAA Paper 2008-0379, Jan. 2008.
    • (2008) AIAA Paper 2008-0379
    • Konrath, R.1    Klein, Ch.2    Schroeder, A.3
  • 20
    • 78149432596 scopus 로고    scopus 로고
    • Experimental and CFD contribution to delta wing vortical flow understanding
    • Jan.
    • LeRoy, J. F., Rodriguez, O. and Kurun, S., "Experimental and CFD Contribution to Delta Wing Vortical Flow Understanding," AIAA Paper 2008-0380, Jan. 2008.
    • (2008) AIAA Paper 2008-0380
    • LeRoy, J.F.1    Rodriguez, O.2    Kurun, S.3
  • 21
    • 78149434544 scopus 로고    scopus 로고
    • Turbulent and unsteady flow characteristics of delta wing vortex systems
    • Jan.
    • Furman, A. and Breitsamter, Ch., "Turbulent and Unsteady Flow Characteristics of Delta Wing Vortex Systems," AIAA Paper 2008-0381, Jan. 2008.
    • (2008) AIAA Paper 2008-0381
    • Furman, A.1    Breitsamter, Ch.2
  • 22
    • 78149442317 scopus 로고    scopus 로고
    • Low speed wind tunnel characterization of the VFE-2 wing
    • Jan.
    • Coton, F., Mat, S. and Galbraith, R., "Low Speed Wind Tunnel Characterization of the VFE-2 Wing," AIAA Paper 2008-0382, Jan. 2008.
    • (2008) AIAA Paper 2008-0382
    • Coton, F.1    Mat, S.2    Galbraith, R.3
  • 23
    • 78149418296 scopus 로고    scopus 로고
    • What was learned from the new VFE-2 experiments?
    • Jan.
    • Luckring, J. M. and Hummel, D., "What was Learned from the New VFE-2 Experiments?," AIAA Paper 2008-0383, Jan. 2008.
    • (2008) AIAA Paper 2008-0383
    • Luckring, J.M.1    Hummel, D.2
  • 24
    • 84878694489 scopus 로고    scopus 로고
    • Semi-empirical prediction of vortex onset and progression on 65° delta wings
    • Jan.
    • Nangia, R. K., "Semi-Empirical Prediction of Vortex Onset and Progression on 65° Delta Wings," AIAA Paper 2008-0384, Jan. 2008.
    • (2008) AIAA Paper 2008-0384
    • Nangia, R.K.1
  • 25
    • 78149423599 scopus 로고    scopus 로고
    • Numerical simulation of the peculiar subsonic flow-field about the VFE-2 delta wing with rounded leading edge
    • Jan.
    • Fritz, W., "Numerical Simulation of the Peculiar Subsonic Flow-Field about the VFE-2 Delta Wing with Rounded Leading Edge," AIAA Paper 2008-0393, Jan. 2008.
    • (2008) AIAA Paper 2008-0393
    • Fritz, W.1
  • 26
    • 78149456323 scopus 로고    scopus 로고
    • Some factors influencing the vortical flow structures on delta wings
    • Jan.
    • Gürdamar, E., Ortakaya, Y., Kaya, S., and Korkem, B., "Some Factors Influencing the Vortical Flow Structures on Delta Wings," AIAA Paper 2008-0394, Jan. 2008.
    • (2008) AIAA Paper 2008-0394
    • Gürdamar, E.1    Ortakaya, Y.2    Kaya, S.3    Korkem, B.4
  • 28
    • 78149460551 scopus 로고    scopus 로고
    • Detached-eddy simulation of the vortical flow field about the VFE-2 delta wing
    • Jan.
    • Cummings, R.M. and Schütte, A., "Detached-Eddy Simulation of the Vortical Flow Field about the VFE-2 Delta Wing. AIAA Paper 2008-0396, Jan. 2008.
    • (2008) AIAA Paper 2008-0396
    • Cummings, R.M.1    Schütte, A.2
  • 29
    • 78149456322 scopus 로고    scopus 로고
    • Steady, subsonic CFD analysis of the VFE-2 configuration and comparison to wind tunnel data
    • Jan.
    • Crippa, S. and Rizzi, A., "Steady, Subsonic CFD Analysis of the VFE-2 Configuration and Comparison to Wind Tunnel Data, "AIAA Paper 2008-0397, Jan. 2008.
    • (2008) AIAA Paper 2008-0397
    • Crippa, S.1    Rizzi, A.2
  • 30
    • 78149463419 scopus 로고    scopus 로고
    • Numerical investigations on the VFE 2 65-degree rounded leading edge delta wing using the unstructured DLR-TAU-code
    • Jan.
    • Schütte, A. and Lüdeke, H., "Numerical Investigations on the VFE 2 65-degree Rounded Leading Edge Delta Wing using the Unstructured DLR-TAU-Code," AIAA Paper 2008-0398, Jan. 2008.
    • (2008) AIAA Paper 2008-0398
    • Schütte, A.1    Lüdeke, H.2
  • 31
    • 78149427429 scopus 로고    scopus 로고
    • What was learned from the numerical simulations for the VFE-2?
    • Jan.
    • Fritz, W. and Cummings, R.M., "What Was Learned from the Numerical Simulations for the VFE-2?," AIAA Paper 2008-0399, Jan. 2008.
    • (2008) AIAA Paper 2008-0399
    • Fritz, W.1    Cummings, R.M.2
  • 32
    • 63349110310 scopus 로고    scopus 로고
    • Prediction of F-16XL flight-flow physics
    • Lamar, J.E., "Prediction of F-16XL Flight-Flow Physics," Journal of Aircraft, Vol. 46, No. 2, 2009, p. 354.
    • (2009) Journal of Aircraft , vol.46 , Issue.2 , pp. 354
    • Lamar, J.E.1
  • 34
    • 63349102583 scopus 로고    scopus 로고
    • Comparison of measured and block structured simulations for the F-16XL aircraft
    • Boelens, O.J., Badcock, K.J., Elmilgui, A., Abdol-Hamid, K.S., Massey, S.J., "Comparison of Measured and Block Structured Simulations for the F-16XL Aircraft," Journal of Aircraft, Vol. 46, No. 2, 2009, pp. 377-384.
    • (2009) Journal of Aircraft , vol.46 , Issue.2 , pp. 377-384
    • Boelens, O.J.1    Badcock, K.J.2    Elmilgui, A.3    Abdol-Hamid, K.S.4    Massey, S.J.5
  • 36
    • 63349105166 scopus 로고    scopus 로고
    • Reynolds-averaged navier-stokes solutions for the CAWAPI F-16XL using different hybrid grids
    • Fritz, W., Davis, M.B., Karman, S.L., Michal; T., "Reynolds-Averaged Navier-Stokes Solutions for the CAWAPI F-16XL Using Different Hybrid Grids," Journal of Aircraft, Vol. 46, No. 2, 2009, pp. 409-422.
    • (2009) Journal of Aircraft , vol.46 , Issue.2 , pp. 409-422
    • Fritz, W.1    Davis, M.B.2    Karman, S.L.3    Michal4    , T.5
  • 37
    • 63349099579 scopus 로고    scopus 로고
    • Lessons learned from numerical simulations of the F-16XL at flight conditions
    • Rizzi, A., Jirasek, A., Lamar, J.E., Crippa, S., Badcock, K.J. and Boelens, O.J., "Lessons Learned from Numerical Simulations of the F-16XL at Flight Conditions," Journal of Aircraft, Vol. 46, No. 2, 2009, pp. 423-441.
    • (2009) Journal of Aircraft , vol.46 , Issue.2 , pp. 423-441
    • Rizzi, A.1    Jirasek, A.2    Lamar, J.E.3    Crippa, S.4    Badcock, K.J.5    Boelens, O.J.6
  • 38
    • 46049109309 scopus 로고    scopus 로고
    • Numerical prediction and wind tunnel experiment for a pitching unmanned combat air vehicle
    • Cummings, R.M., Morton, S.A., and Siegel, S.G., "Numerical Prediction and Wind Tunnel Experiment for a Pitching Unmanned Combat Air Vehicle," Aerospace Science and Technology, Vol. 12, Issue 5, 2008, pp. 355-364.
    • (2008) Aerospace Science and Technology , vol.12 , Issue.5 , pp. 355-364
    • Cummings, R.M.1    Morton, S.A.2    Siegel, S.G.3
  • 40
    • 0033133176 scopus 로고    scopus 로고
    • Dynamic stall of pitching airfoils and delta wings, similarities and differences
    • Ericsson, L.E., "Dynamic Stall of Pitching Airfoils and Delta Wings, Similarities and Differences," Journal of Aircraft, Vol. 36, No. 3, 1999, pp. 603-605.
    • (1999) Journal of Aircraft , vol.36 , Issue.3 , pp. 603-605
    • Ericsson, L.E.1
  • 41
    • 84964291070 scopus 로고    scopus 로고
    • Time accurate euler calculations of vortical flow on a delta wing in pitching motion
    • June-July
    • Arthur, M.T., Brandsma, F., Ceresola, N., Kordulla, W., "Time Accurate Euler Calculations of Vortical Flow on a Delta Wing in Pitching Motion," AIAA Paper 99-3110, June-July 1999.
    • (1999) AIAA Paper 99-3110
    • Arthur, M.T.1    Brandsma, F.2    Ceresola, N.3    Kordulla, W.4
  • 42
    • 0028539557 scopus 로고
    • Navier-stokes prediction of large-amplitude delta-wing roll oscillations
    • Chaderjian, N.M., "Navier-Stokes Prediction of Large-Amplitude Delta-Wing Roll Oscillations," Journal of Aircraft, Vol. 31, No. 6, 1990, pp. 1333-1340.
    • (1990) Journal of Aircraft , vol.31 , Issue.6 , pp. 1333-1340
    • Chaderjian, N.M.1
  • 43
    • 0029705058 scopus 로고
    • Numerical simulation of forced and free-to-roll delta-wing motions
    • Chaderjian, N.M. and Schiff, L.B., "Numerical Simulation of Forced and Free-to-Roll Delta-Wing Motions," Journal of Aircraft, Vol. 33, No. 1, 1992, pp. 93-99.
    • (1992) Journal of Aircraft , vol.33 , Issue.1 , pp. 93-99
    • Chaderjian, N.M.1    Schiff, L.B.2
  • 44
    • 85001754699 scopus 로고
    • Roll-induced cross-loads on a delta wing at high incidence
    • Sep.
    • Hanff, E.S. and Huang, X.Z., "Roll-Induced Cross-Loads on a Delta Wing at High Incidence," AIAA Paper 91-3223, Sep. 1991.
    • (1991) AIAA Paper 91-3223
    • Hanff, E.S.1    Huang, X.Z.2
  • 45
    • 78649502061 scopus 로고    scopus 로고
    • Low speed wind tunnel experiments on a delta wing oscillating in pitch
    • Hummel, D. and Löser, T., "Low Speed Wind Tunnel Experiments on a Delta Wing Oscillating in Pitch," ICAS Paper 98-3.9.3, 1998.
    • (1998) ICAS Paper 98-3.9.3
    • Hummel, D.1    Löser, T.2
  • 48
    • 78349291902 scopus 로고    scopus 로고
    • Modeling of natural transition in properly three-dimensional flows
    • June
    • Arthur, M. and Mughal, M., "Modeling of Natural Transition in Properly Three-Dimensional Flows," AIAA Paper 2009-3556, June 2009.
    • (2009) AIAA Paper 2009-3556
    • Arthur, M.1    Mughal, M.2
  • 50
    • 34250726149 scopus 로고    scopus 로고
    • CFD analysis of the low-speed aerodynamic characteristics of a UCAV
    • Jan.
    • Petterson, K., "CFD Analysis of the Low-Speed Aerodynamic Characteristics of a UCAV," AIAA Paper 2006-1259, Jan. 2006.
    • (2006) AIAA Paper 2006-1259
    • Petterson, K.1
  • 51
    • 33845416887 scopus 로고    scopus 로고
    • Low-speed aerodynamic and flow field characteristics of a UCAV
    • June
    • Petterson, K., "Low-Speed Aerodynamic and Flow field Characteristics of a UCAV," AIAA Paper 2006-2986, June 2006.
    • (2006) AIAA Paper 2006-2986
    • Petterson, K.1
  • 52
    • 33845420729 scopus 로고    scopus 로고
    • Joint TTCP CFD studies into the 1303 UCAV performance: First year results
    • June
    • Wong, M.D., "Joint TTCP CFD Studies into the 1303 UCAV Performance: First Year Results," AIAA Paper 2006-2984, June 2006.
    • (2006) AIAA Paper 2006-2984
    • Wong, M.D.1
  • 53
    • 35648962361 scopus 로고    scopus 로고
    • A computational study of the low-speed flow over the 1303 UCAV configuration
    • June
    • Arthur, M.T. and Petterson, K., "A Computational Study of the Low-Speed Flow over the 1303 UCAV Configuration," AIAA Paper 2007-4568, June 2007.
    • (2007) AIAA Paper 2007-4568
    • Arthur, M.T.1    Petterson, K.2
  • 54
    • 78549246833 scopus 로고    scopus 로고
    • Computational study of reynolds number and angle-of-attack effects on a 1303 UCAV configuration with a high-order overset-grid algorithm
    • Jan.
    • Sherer, S.E., Visbal M.R., and Gordnier, R.E., "Computational Study of Reynolds Number and Angle-of-Attack Effects on a 1303 UCAV Configuration with a High-Order Overset-Grid Algorithm," AIAA Paper 2009-0751, Jan. 2009.
    • (2009) AIAA Paper 2009-0751
    • Sherer, S.E.1    Visbal, M.R.2    Gordnier, R.E.3
  • 56
    • 42949086397 scopus 로고    scopus 로고
    • Ground-based simulation of complex maneuvers of a delta wing aircraft
    • Rein, M., Höhler, G., Schütte, A., Bergmann, A., Löser, T., "Ground-Based Simulation of Complex Maneuvers of a Delta Wing Aircraft," Journal of Aircraft, Vol. 45, No. 1, 2008, pp. 286-291.
    • (2008) Journal of Aircraft , vol.45 , Issue.1 , pp. 286-291
    • Rein, M.1    Höhler, G.2    Schütte, A.3    Bergmann, A.4    Löser, T.5
  • 61
    • 34547498301 scopus 로고    scopus 로고
    • Numerical design of a low-noise high-lift system for a supersonic aircraft
    • Berlin: Springer-Verlag
    • Herrmann, U., "Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft," Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 92, Berlin: Springer-Verlag, 2006.
    • (2006) Notes on Numerical Fluid Mechanics and Multidisciplinary Design , vol.92
    • Herrmann, U.1
  • 64
    • 39149139328 scopus 로고    scopus 로고
    • Experimental and numerical research on the aerodynamics of unsteady moving aircraft
    • Bergmann, A., Hübner, A.-R., and Löser, T., "Experimental and numerical research on the aerodynamics of unsteady moving aircraft," Progress in Aerospace Sciences, Vol. 44, Issue 2, 2008, pp. 121-137.
    • (2008) Progress in Aerospace Sciences , vol.44 , Issue.2 , pp. 121-137
    • Bergmann, A.1    Hübner, A.-R.2    Löser, T.3
  • 65
    • 0343863938 scopus 로고
    • On the dynamics of short pressure probes: Some design factors affecting frequency response
    • Nyland, T.W., Englund, D.R., and Anderson, R.C., "On The Dynamics of Short Pressure Probes: Some Design Factors Affecting Frequency Response," NASA TN D-6151 (1971).
    • (1971) NASA TN D-6151
    • Nyland, T.W.1    Englund, D.R.2    Anderson, R.C.3
  • 66
    • 85067320294 scopus 로고    scopus 로고
    • CFD analysis of the flow around the X-31 aircraft at high angle of attack
    • June
    • Boelens, O.J., "CFD Analysis of the Flow Around the X-31 Aircraft at High Angle of Attack," AIAA Paper 2009-3628, June 2009.
    • (2009) AIAA Paper 2009-3628
    • Boelens, O.J.1
  • 67
    • 85067318961 scopus 로고    scopus 로고
    • Application of volterra functions to X-31 aircraft model motion
    • June
    • Jirasek, A. and Cummings, R.M., "Application of Volterra Functions to X-31 Aircraft Model Motion," AIAA Paper 2009-3629, June 2009.
    • (2009) AIAA Paper 2009-3629
    • Jirasek, A.1    Cummings, R.M.2
  • 68
    • 78649496696 scopus 로고    scopus 로고
    • SACCON static wind tunnel tests at DNW- NWB and 14'×22' NASA LaRC
    • June
    • Löser, T., Vicroy, D., and Schütte, A., "SACCON Static Wind Tunnel Tests at DNW- NWB and 14'×22' NASA LaRC," AIAA Paper 2010-4393, June 2010.
    • (2010) AIAA Paper 2010-4393
    • Löser, T.1    Vicroy, D.2    Schütte, A.3
  • 69
    • 84878684374 scopus 로고    scopus 로고
    • SACCON dynamic wind tunnel tests at DNW- NWB and 14'×22' NASA LaRC
    • June
    • Vicroy, D. and Löser, T., "SACCON Dynamic Wind Tunnel Tests at DNW- NWB and 14'×22' NASA LaRC," AIAA Paper 2010-4394, June 2010.
    • (2010) AIAA Paper 2010-4394
    • Vicroy, D.1    Löser, T.2
  • 70
    • 78649515447 scopus 로고    scopus 로고
    • Static and dynamic SACCON PIV tests - Part I: Forward flowfield
    • June
    • Gilliott, A., "Static and Dynamic SACCON PIV Tests - Part I: Forward Flowfield," AIAA Paper 2010-4395, June 2010.
    • (2010) AIAA Paper 2010-4395
    • Gilliott, A.1
  • 73
    • 78649519336 scopus 로고    scopus 로고
    • Strategy for dynamic CFD simulations on SACCON configuration
    • June
    • Frink, N., "Strategy for Dynamic CFD Simulations on SACCON Configuration," AIAA Paper 2010-4559, June 2010.
    • (2010) AIAA Paper 2010-4559
    • Frink, N.1
  • 75
    • 78649501751 scopus 로고    scopus 로고
    • Computational study of static and dynamic vortical flow over the delta wing SACCON configuration using the FOI flow solver edge
    • June
    • Tormalm, T., Tomac, M., and Schmidt, S., "Computational Study of Static And Dynamic Vortical Flow over the Delta Wing SACCON Configuration Using the FOI Flow Solver Edge," AIAA Paper 2010-4561, June 2010.
    • (2010) AIAA Paper 2010-4561
    • Tormalm, T.1    Tomac, M.2    Schmidt, S.3
  • 76
    • 78649499187 scopus 로고    scopus 로고
    • SACCON CFD static and dynamic derivatives using ElsA
    • June
    • LeRoy, J., "SACCON CFD Static and Dynamic Derivatives Using elsA," AIAA Paper 2010-4562, June 2010.
    • (2010) AIAA Paper 2010-4562
    • LeRoy, J.1
  • 78
    • 78649527907 scopus 로고    scopus 로고
    • Numerical and experimental analyses of the vortical flow around the SACCON configuration
    • June
    • Schütte, A., Hummel, D., and Hitzel, S., "Numerical and Experimental Analyses of the Vortical Flow Around the SACCON Configuration," AIAA Paper 2010-4690, June 2010.
    • (2010) AIAA Paper 2010-4690
    • Schütte, A.1    Hummel, D.2    Hitzel, S.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.