Publications by Raffaello Mariani
Peer reviewed
Articles
[1]
S. Suewatanakul et al., "Conceptual Design of a Hybrid Hydrogen Fuel Cell/Battery Blended-Wing-Body Unmanned Aerial Vehicle—An Overview," Aerospace, vol. 9, no. 5, pp. 275-275, 2022.
[2]
X. F. Wei et al., "Experimental Investigations of Screech Mitigation and Amplification by Beveled and Double-Beveled Nozzles," Journal of Aerospace Engineering, vol. 35, no. 4, 2022.
[3]
X. F. Wei et al., "Near- and Far-Field Acoustic Measurements for Stepped Nozzles at Over- and Perfectly-Expanded Supersonic Jet Flow Conditions," Journal of Fluids Engineering, vol. 142, no. 11, 2020.
[4]
R. Mariani et al., "On the application of non-standard rainbow schlieren technique upon supersonic jets," Journal of Visualization, vol. 23, no. 3, pp. 383-393, 2020.
[5]
H. D. Lim et al., "Short-time proper orthogonal decomposition of time-resolved schlieren images for transient jet screech characterization," Aerospace Science and Technology, vol. 107, 2020.
[6]
R. Mariani et al., "A comparative study on the use of calibrated and rainbow schlieren techniques in axisymmetric supersonic jets," Flow Measurement and Instrumentation, vol. 66, pp. 218-228, 2019.
[7]
H. Lim et al., "Effects of bevelled nozzles on standoff shocks in supersonic impinging jets," Aerospace Science and Technology, vol. 94, 2019.
[8]
X. F. Wei et al., "Mitigation of under-expanded supersonic jet noise through stepped nozzles," Journal of Sound and Vibration, vol. 459, 2019.
[9]
H. Lim et al., "Visual-hull based 3D reconstruction of shocks in under-expanded supersonic bevelled jets.," Experimental Thermal and Fluid Science, vol. 99, pp. 458-473, 2018.
[10]
R. Jesudasan, A. Hanifi and R. Mariani, "Investigating Planar and Nonplanar Wing Planform Optimisation for Ground Effect Aircraft," Aerospace, vol. 10, no. 11, 2017.
[11]
R. Mariani, K. Kontis and N. Gongora-Orozco, "Head On Collisions of Compressible Vortex Rings on a Smooth Solid Surface. : Effects of Surface Distance Variation.," Shock Waves, 2013.
[12]
R. Mariani et al., "Shock-Free Compressible Vortex Rings Impinging on a Stationary Surface: Effects of Surface Angle Variation.," Experimental Thermal and Fluid Science, vol. 47, pp. 126-142, 2013.
[13]
R. Mariani, M. K. Quinn and K. Kontis, "A Note on the Generation of a Compressible Vortex Rings Using Helium as Driver Gas.," Proceedings of the Institution of Mechanical Engineers. Part G, Journal of Aerospace Engineering, vol. 227, no. 10, pp. 1637-1645, 2012.
[14]
R. Mariani and K. Kontis, "Experimental Studies on Coaxial Vortex Loops," Physics of fluids, vol. 22, no. 12, 2010.
[15]
D. Landman et al., "Hybrid Design for Aircraft Wind-Tunnel Testing Using Response Surface Methodology," Journal of Aircraft, vol. 44, no. 4, pp. 1214-1221, 2007.
Conference papers
[16]
C. Neves and R. Mariani, "Flow Control on a Swept Wing Using Aerodynamically Shaped Vortex Generators," in AIAA SciTech Forum and Exposition, 2024, 2024.
[17]
C. Neves, C. Gennari and R. Mariani, "Stall Development Control Using a Bio-InspiredLeading-Edge Design," in Aerospace Europe Conference 2023 - 10th EUCASS - 9th CEAS, Lausanne, Switzerland, July 9-13, 2023, 2023.
[18]
V. N. Fernandez-Ayala et al., "DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING," in 33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022, 2022, pp. 1078-1087.
[19]
R. Jesudasan, R. Mariani and A. Hanifi, "PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT," in 33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022, 2022, pp. 3106-3118.
[20]
R. Mariani et al., "WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE," in 33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022, 2022, pp. 2711-2721.
[21]
R. Mariani et al., "A Preliminary Study On the Implementation of Rainbow Schlieren with a Single-Mirror System," in Proc. of the 32nd International Symposium on Shock Waves, 2019.
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2024-05-31 00:16:40