AADL Logo Advanced Aircraft Design Lab

Royal Military College of Canada

Publications

Journal Articles

Conference Proceedings

Conference Presentartions


AAP19

W.D.E. Allan, A. Asghar, and R.E. Perez. Application of bio-inspired leading-edge features to enhance propeller performance in air vehicles. In AIAA Scitech Forum, number AIAA 2019-0851. San Diego, CA, January 7-11 2019. doi:10.2514/6.2018-3647.

AP12

S. Andrews and R.E. Perez. Sizing of a short range civil transport aircraft considering aero-structural and stability effects. In 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSM Multidisciplinary Analysis and Optimization Conference, number AIAA 2012-5589. Indianapolis, Indiana, September 17-19 2012. doi:10.2514/6.2012-5589.

AP13

S. Andrews and R.E. Perez. Design of nonplanar regional jet aircraft considering aero-structural and stability couplings. In CASI AERO Conference. Toronto, ON, May 30 - June 2 2013.

AP14

S. Andrews and R.E. Perez. Stability and control effects on the design optimization of a box-wing aircraft. In AVIATION 2014, 14th AIAA Aviation Technology, Integration, and Operations Conference, number AIAA 2014-2592. Atlanta, GA, June 16-20 2014. doi:10.2514/6.2014-2592.

AP15a

S. Andrews and R.E. Perez. Multidisciplinary analysis of a box-wing aircraft designed for a regional-jet mission. In AVIATION 2015, 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, number AIAA 2015-2793. Dallas, TX, June 22-26 2015. doi:10.2514/6.2015-2793.

AP15b

S. Andrews and R.E. Perez. Parametric study of box-wing aerodynamics for minimum drag under stability and maneuverability constraints. In AVIATION 2015, 33rd AIAA Applied Aerodynamics Conference, number AIAA 2015-3291. Dallas, TX, June 22-26 2015. doi:10.2514/6.2015-3291.

AP17

S. Andrews and R.E. Perez. Analytic study of the conditions required for longitudinal stability of dual-wing aircraft. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, May 2017. doi:10.1177/0954410017704215.

AP18

S. Andrews and R.E. Perez. Comparison of box-wing and conventional aircraft mission performance using multi-disciplinary analysis and optimization. Aerospace Science and Technology, 79:336–351, 2018. doi:10.1016/J.AST.2018.05.060.

APA13

S. Andrews, R.E. Perez, and W. Allan. Aerodynamic implications of gull's drooped wing-tips. Bioinspiration & Biomimetics, 8(4):1–13, December 2013. doi:10.1088/1748-3182/8/4/046003.

APA15

S. Andrews, R.E. Perez, and W.D.E. Allan. The drooped wings of gulls: aerodynamic optimum or kinematic constraint? In CASI AERO Conference. 2015.

APW15

S.A. Andrews, R.E. Perez, and D. Wowk. Wing weight model for conceptual design of nonplanar configurations. Aerospace Science and Technology, 43:51–62, 2015. doi:http://dx.doi.org/10.1016/j.ast.2015.02.011.

APA18

A. Asghar, R.E. Perez, and W.D.E. Allan. Application of leading edge tubercles to enhance propeller performance. In AIAA Aviation Forum, Applied Aerodynamics Conference, number AIAA 2018-3647. Atlanta, Georgia, June 25-29 2018. doi:10.2514/6.2018-3647.

APA19

A. Asghar, R.E. Perez, and W.D.E. Allan. Further parametric investigation of leading-edge tubercles on the propeller performance. In AIAA Scitech Forum, number AIAA 2019-0850. San Diego, CA, January 7-11 2019. doi:10.2514/6.2019-0850.

APF17

A. Asghar, R.E. Perez, and M. Ferchichi. Effect of leading edge tubercles on transonic performance of airfoils. In AIAA AVIATION Conference, 35th AIAA Applied Aerodynamics Conference, number AIAA 2017-3402. Denver, CO, June 5-9 2017. doi:10.2514/6.2017-3402.

APF18

A. Asghar, R.E. Perez, and M. Ferchichi. Transonic performance of airfoils using leading edge tubercles. In 53rd 3AF International Conference on Applied Aerodynamics. Salon de Provence, France, March 26-28 2018.

APJA19

A. Asghar, R.E. Perez, P.W. Jansen, and W.D.E. Allan. Effect of leading edge tubercles on performance of propellers. In CASI AERO Conference. Montreal, QC, May 2019.

APJA20

A. Asghar, R.E. Perez, P.W. Jansen, and W.D.E. Allan. Application of leading-edge tubercles to enhance propeller performance. AIAA Journal, September 2020. 4656-4671. doi:10.2514/1.J058740.

CP22

R. Colpitts and R.E. Perez. Application of leading edge tubercles on rotor blades, in press. AIAA Journal, 2022.

CPJLB20

R. Colpitts, R.E. Perez, P.W. Jansen, and A. Levert-Beaulieu. Effect of target lift coefficient on aerodynamic optimization of transonic leading edge tubercles. In AIAA Scitech 2020 Forum, number AIAA-2020-1542. Orlando, FL, 6-10 January 2020. doi:10.2514/6.2020-1542.

CDP22

R.R. Colpitts, Hesketh D., and R.E. Perez. Experimental characterization of leading edge tubercles on rotor blades. In AIAA Scitech 2022 Forum, number AIAA-2022-1966. San Diego, CA, 03-07 January 2022. doi:10.2514/6.2022-1966.

CLBRE21

R.R. Colpitts, A. Levert-Beaulieu, and Perez R.E. Effect of various cambered airfoil profiles to wings with leading edge tubercles in transonic flow. In AIAA Scitech 2021 Forum, number AIAA-2021-0468. Virtual Event, 19-21 January 2021. doi:10.2514/6.2021-0468.

CNP21

R.R. Colpitts, M. Nayman, and R.E. Perez. Optimization of leading edge tubercles applied to helicopter rotor blades. In AIAA Scitech 2021 Forum, number AIAA-2021-0733. Virtual Event, 19-21 January 2021. doi:10.2514/6.2021-0733.

CPJ20

R.R. Colpitts, R.E. Perez, and P.W. Jansen. Effect of leading-edge tubercles on rotor blades. In AIAA AVIATION 2020 FORUM, number AIAA-2020-2763. Virtual Event, June 2020. doi:10.2514/6.2020-2763.

DFPB16

M. Dghim, M. Ferchichi, R.E. Perez, and M. BenChiekh. Near wake development of a wing tip vortex under the effect of synthetic jet actuation. Aerospace Science and Technology, 54:88–107, July 2016. doi:10.1016/j.ast.2016.04.008.

GGPJ18

O. Gonzalez-Gallego, R.E. Perez, and P.W. Jansen. Technical viability and operational assessment of a supersonic business jet. In AIAA Aviation Forum, Aviation Technology, Integration, and Operations Conference, number AIAA 2018-3661. Atlanta, Georgia, June 25-29 2018. doi:10.2514/6.2018-3661.

HMP12

R. Henderson, J.R.R.A. Martins, and R.E. Perez. Aircraft conceptual design for optimal environmental performance. Aeronautical Journal, 116(1175):1–22, 2012. doi:10.1017/S000192400000659X.

HPJD22

D. Hesketh, R.E. Perez, P.W. Jansen, and L. Diatchencko. Analysis of leading edge tubercles applied to vertical axis wind turbines. In AIAA AVIATION Forum, number AIAA-2022-3891. Chicago, IL, July 27 - July 1 2022. doi:10.2514/6.2022-3891.

JP14

P. W. Jansen and R. E. Perez. Robust coupled optimization of aircraft design and fleet allocation for multiple markets. In AVIATION 2014, AIAA/3AF Aircraft Noise and Emissions Reduction Symposium, number AIAA 2014-2735. Atlanta, GA, June 16-20 2014. doi:10.2514/6.2014-2735.

JP16a

P. W. Jansen and R. E. Perez. Integrated design and optimization of aircraft families and air transport network. In AIAA AVIATION 2016 Conference, number AIAA-2016-3748. Washington, DC, 13-17 June 2016. doi:10.2514/6.2016-3748.

JP10

P.W. Jansen and R.E. Perez. Effect of size and mission requirements on the design optimization of non-planar aircraft configurations. In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization (MAO) Conference, number AIAA 2010-9188. Fort Worth, Texas, September 13-15 2010. doi:10.2514/6.2010-9188.

JP11a

P.W. Jansen and R.E. Perez. Constrained structural design optimization via a parallel augmented lagrangian particle swarm optimization approach. International Journal of Computer and Structures, 89(13-14):1352–1366, July 2011. doi:10.1016/j.compstruc.2011.03.011.

JP11b

P.W. Jansen and R.E. Perez. Coupled optimization of aircraft family design and fleet assignment. In 58th CASI Aeronautics Conference, Aircraft Design and Development Symposium. Montreal, Quebec, April 26-28 2011.

JP12

P.W. Jansen and R.E. Perez. Coupled optimization of aircraft family design and fleet assignment for minimum cost and fuel burn. In 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSM Multidisciplinary Analysis and Optimization Conference, number AIAA 2012-5495. Indianapolis, Indiana, September 17-19 2012. doi:10.2514/6.2012-5495.

JP13a

P.W. Jansen and R.E. Perez. Cost prediction and optimization of an aircraft family. In CASI AERO Conference. Toronto, ON, May 30 - June 2 2013.

JP13b

P.W. Jansen and R.E. Perez. Coupled optimization of aircraft design and fleet allocation with uncertain passenger demand. In AVIATION 2013, Aviation Technology, Integration, and Operations Conference, number AIAA 2013-4392. Los Angeles, CA, August 12-14 2013. doi:10.2514/6.2013-4392.

JP15

P.W. Jansen and R.E. Perez. Simultaneous optimization of aircraft family design and fleet allocation on multiple markets for economic and environmental considerations. In CASI AERO Conference. 2015.

JP16b

P.W. Jansen and R.E. Perez. Coupled optimization of aircraft families and fleet allocation for multiple markets. AIAA Journal of Aircraft, 53(5):1485–1504, 2016. doi:10.2514/1.C033646.

JP17a

P.W. Jansen and R.E. Perez. Effect of passenger preferences on the integrated design and optimization of aircraft families and air transport network. In AIAA AVIATION Conference, 17th AIAA Aviation Technology, Integration, and Operations Conference, number AIAA 2017-4249. Denver, CO, June 5-9 2017. doi:10.2514/6.2017-4249.

JP17b

P.W. Jansen and R.E. Perez. System of systems design optimization of aircraft families and air transport network. In CASI AERO Conference. 2017.

JP19

P.W. Jansen and R.E. Perez. Multi-objective design optimization of an mom aircraft using an asynchronous constrained pso. In AIAA Scitech Forum, number AIAA 2019-0008. San Diego, CA, January 7-11 2019. doi:10.2514/6.2019-0008.

JPM10

P.W. Jansen, R.E. Perez, and J.R.R.A. Martins. Aerostructural optimization of nonplanar lifting surfaces. AIAA Journal of Aircraft, 47(5):1490–1503, September-October 2010. doi:10.2514/1.44727.

KP22

E. J. Kim and R.E. Perez. Robust neurocontrol for autonomous dynamic soaring. In AIAA Scitech 2022 Forum, number AIAA-2022-1417. San Diego, CA, 03-07 January 2022. doi:10.2514/6.2022-1417.

KP21a

E.J. Kim and R.E. Perez. Neuroevolutionary control for autonomous soaring. MDPI Aerospace Journal, September 2021. doi:10.3390/aerospace8090267.

KP21b

Eric J. Kim and Ruben E. Perez. Neural network-based robust dynamic soaring. In CASI AERO 2021. 2021.

KTP21

Noah J. Kurus, Timothy T. Takahashi, and Ruben E. Perez. Critical mach number predictive methods for realistic supersonic wing / body configurations. In AIAA AVIATION 2021 FORUM. 2021. doi:10.2514/6.2021-2432.

LP12

M. LaViolette and R.E. Perez. On the prediction of pollutant emission indices from gas turbine combustion chambers. In ASME Turbo Expo, number GT2012-70038. Copenhagen, Denmark, June 11-15 2012. doi:10.1115/GT2012-70038.

LPA+17

S. Leithead, R.E. Perez, W.D.E. Allan, P.W. Jansen, and T. Connerty. Designing an aircraft in an undergraduate team environment: how 4th year rmc aeronautical engineering students learn by designing and doing. In CASI AERO Conference. 2017.

LBPA19

A. Levert-Beaulieu, R.E. Perez, and A. Asghar. Optimization and experimental characterization of leading edge tubercles in transonic flow. In CASI AERO Conference. Montreal, QC, May 2019.

LBPJ19

A. Levert-Beaulieu, R.E. Perez, and P.W. Jansen. Euler-based aerodynamic shape optimization of leading edge tubercles in transonic flow. In AIAA Scitech Forum, number AIAA-2019-0852. San Diego, CA, January 7-11 2019. doi:10.2514/6.2019-0852.

MMP10

S. Markin, J. K. Mills, and R.E. Perez. Multiple specification longitudinal control of a mini flying wing uav. In The Canadian Society for Mechanical Engineering Forum. Victoria, BC, Canada, June 7-9 2010.

MPJ19

R.J. Mehta, R.E. Perez, and P.W. Jansen. Aerodynamic characteristics of tubercled slotted flaps. In AIAA Aviation 2019 Forum, number AIAA-2019-3295. Dallas, TX, 17-21 June 2019. doi:10.2514/6.2019-3295.

MPA19

R.M. Mehta, R.E. Perez, and A. Asghar. Aerodynamic characteristics of tubercled slotted flaps. In CASI AERO Conference. Montreal, QC, May 2019.

NP22

M. Nayman and R.E. Perez. Improving dynamic stall effects using leading edge tubercles. In AIAA AVIATION Forum, number AIAA-2022-3529. Chicago, IL, July 27 - July 1 2022. doi:10.2514/6.2022-3529.

OPJ17

Gonzalez-Gallego O., R.E. Perez, and P.W. Jansen. Technology drivers for a commercialy viable supersonic business jet. In CASI AERO Conference. 2017.

PAJ20

R.E. Perez, J. Arnal, and P.W. Jansen. Neuro-evolutionary control for optimal dynamic soaring. In AIAA Scitech 2020 Forum, number AIAA-2020-1946. Orlando, FL, 6-10 January 2020. doi:10.2514/6.2020-1946.

PA19(1,2)

R.E. Perez and J.H. Arnal. Dynamic soaring using a \\ neuro-evolutionary approach. In CASI AERO Conference. Montreal, QC, May 2019.

PA18

R.E. Perez and A. Asghar. Numerical study of the effects of leading edge tubercles on transonic performance of airfoils. In AIAA Aviation Forum, Applied Aerodynamics Conference, number AIAA 2018-3955. Atlanta, Georgia, June 25-29 2018. doi:10.2514/6.2018-3955.

PJ11(1,2)

R.E. Perez and P. Jansen. Aero-structural optimization of non-planar lifting configurations for large regional and business jets. In 58th CASI Aeronautics Conference, Aircraft Design and Development Symposium. Montreal, Quebec, April 26-28 2011.

PJM12

R.E. Perez, P. Jansen, and J.R.R.A. Martins. PyOpt: a python-based object-oriented framework for nonlinear constrained optimization. Structures and Multidisciplinary Optimization, 45(1):101–118, 2012. doi:10.1007/s00158-011-0666-3.

PJ14

R.E. Perez and P.W. Jansen. Design optimization and staging assignment for long-range aircraft operations. In AVIATION 2014, AIAA/3AF Aircraft Noise and Emissions Reduction Symposium, number AIAA 2014-2732. Atlanta, GA, June 16-20 2014. doi:10.2514/6.2014-2732.

PJ17a

R.E. Perez and P.W. Jansen. Coupled aircraft design and staging assignment for long range operations. Journal of Aerospace Operations, pages 1–21, August 2017. doi:10.3233/AOP-170064.

PJ17b

R.E. Perez and P.W. Jansen. Coupled design optimization of aircraft and intermediate stop operations assignment on long-range routes. In CASI AERO Conference. 2017.

PMCA12

R.E. Perez, C. Marsden, T. Chalovich, and W. Allan. Implementing a capstone aircraft design project as an integrated multi-disciplinary development experience. In 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSM Multidisciplinary Analysis and Optimization Conference, number AIAA 2012-5407. Indianapolis, Indiana, September 17-19 2012. doi:10.2514/6.2012-5407.

PM08

R.E. Perez and J.R.R.A. Martins. PyACDT: an object-oriented framework for aircraft design modelling and multidisciplinary optimization. In 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, number AIAA 2008-5955. Victoria, BC, September 10 - 12 2008. doi:10.2514/6.2008-5955.

PP17

L. Peristy and R.E. Perez. Modelling wakes and flight dynamics using aerodynamic adjoints for air-to-air refueling. In CASI AERO Conference. 2017.

PP22

L. Peristy and R.E. Perez. Examination of the dynamic modes of a single-seater fighter jet during aerial refuelling. In CEAS EuroGNC 2022. Berlin, Germany, May 3-5 2022.

PPAA17

L. Peristy, R.E. Perez, A. Asghar, and W.D.E. Allan. Aerodynamic characterization of leading edge protuberances at various reynolds numbers. In CASI AERO Conference. 2017.

PPJ19a

L. Peristy, R.E. Perez, and P.W. Jansen. Wake modelling with embedded lateral and directional stability sensitivity analysis for aerial refuelling or formation flight. In AIAA Scitech Forum, number AIAA 2019-0583. AIAA Scitech Forum, January 7-11 2019. doi:10.2514/6.2019-0583.

PPJ19b(1,2)

L. Peristy, R.E. Perez, and P.W. Jansen. Wake modelling with prediction of handling qualities for air-to-air refueling. In CASI AERO Conference. Montreal, QC, May 2019.

PPAA16

L. H. Peristy, R. E. Perez, A. Asghar, and W. D. Allan. Reynolds number effect of leading edge tubercles on airfoil aerodynamics. In AIAA AVIATION 2016 Conference, 36th AIAA Applied Aerodynamics Conference, number AIAA 2016-3260. Washington, DC, 13-17 June 2016. doi:10.2514/6.2016-3260.

PPJ18

L.H. Peristy, R.E. Perez, and P.W. Jansen. Wake modelling for aerial refuelling using aerodynamic adjoints. In AIAA SciTech Forum. Kissimmee, Florida, January 8-12 2018. doi:10.2514/6.2018-1758.

PPJ20

L.H. Peristy, R.E. Perez, and P.W. Jansen. Flying qualities prediction tool for aerial refuelling operational compatibility assessment. In AIAA Scitech 2020 Forum, number AIAA-2020-1261. Orlando, FL, 6-10 January 2020. doi:10.2514/6.2020-1261.

RPA19a

S. J. Reid, R.E. Perez, and A. Asghar. Characterization of finite tubercle wings. In CASI AERO Conference. Montreal, QC, May 2019.

RPA19b

S.J. Reid, R.E. Perez, and A. Asghar. Characterization of tubercle effects on finite span wings. In AIAA Aviation 2019 Forum, number AIAA-2019-3294. Dallas, Texas, 17-21 June 2019. doi:10.2514/6.2019-3294.

RPJB21

S.J. Reid, R.E. Perez, P.W. Jansen, and C. Bil. Influence of carbon pricing on regional aircraft and route network design. In AIAA Scitech 2021 Forum, number AIAA-2021-0463. Virtual Event, 19-21 January 2021. doi:10.2514/6.2021-0463.

RPJ21

Stewart Reid, Ruben E. Perez, and Peter W. Jansen. Turboprop design analysis in regional route networks consideringcarbon pricing economics. In CASI AERO 2021. June 2021.

RP09

Z. Richards and R.E. Perez. Study of particle swarm optimization formulations for the solution of constrained nonlinear optimization problems. In Annual Meeting of the Society of the Industrial and Applied Mathematics (SIAM). Denver, CO, July 6-10 2009.

SLP10

Y. Saeedi, H. T. Liu, and R.E. Perez. Robustness analysis of a simultaneously stabilizing controller: a flight control case study. In AIAA Guidance, Navigation, and Control Conference, number AIAA 2010-8336. Toronto, ON, Canada, August 2-5 2010. doi:10.2514/6.2010-8336.

SPAA20

S.S. Sidhu, R.E. Perez, W.D. Allan, and A. Asghar. Novel parameters for the performance evaluations of leading edge tubercles on airfoils. In AIAA AVIATION 2020 FORUM, number AIAA-2020-2691. Virtual Event, June 2020. doi:10.2514/6.2020-2691.

SCPA22

F. Sim, R. Colpitts, R.E. Perez, and A. Asghar. Effect of leading edge tubercles on tilt-wing transition. In AIAA AVIATION Forum, number AIAA-2022-3518. Chicago, IL, July 27 - July 1 2022. doi:10.2514/6.2022-3518.

TP20a

T.T. Takahashi and R.E. Perez. On the operational implications of traditional design rules for minimum controllable airspeed. In AIAA Scitech 2020 Forum, number AIAA-2020-0749. Orlando, FL, 6-10 January 2020. doi:10.2514/6.2020-0749.

TP20b

T.T. Takahashi and R.E. Perez. The effect of manufacturing variation on aerodynamic performance and flight safety. In AIAA AVIATION 2020 FORUM, number AIAA-2020-2649. Virtual Event, June 2020. doi:10.2514/6.2020-2649.

TP21

T.T. Takahashi and R.E. Perez. The assumed wind procedure to increase dispatch safety for vmca limited aircraft. In AIAA Scitech 2021 Forum, number AIAA-2021-0459. Virtual Event, 19-21 January 2021. doi:10.2514/6.2021-0459.

YJP12

B. Yan, P.W. Jansen, and R.E. Perez. Multidisciplinary design optimization of airframe and trajectory considering cost and emissions. In 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSM Multidisciplinary Analysis and Optimization Conference, number AIAA 2012-5494. Indianapolis, Indiana, September 17-19 2012. doi:10.2514/6.2012-5494.

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