Comparative assessment of modified deconvolution and neuro-fuzzy technique for force prediction using an accelerometer balance system
Tài liệu tham khảo
Simmons, 1991, Drag balance for hypervelocity impulse facilities, AIAA. J., 29, 2185, 10.2514/3.10858
Naumann, 1991, Technique for aerodynamic force measurement within milliseconds in shock tunnel, Shock Waves., 1, 223, 10.1007/BF01413797
Tanno, 2012, Free-flight force measurement technique in shock tunnel
Sahoo, 2003, An accelerometer balance system for measurement of aerodynamic force coefficients over blunt bodies in a hypersonic shock tunnel, Meas. Sci. Technol., 14, 260, 10.1088/0957-0233/14/3/303
Mee, 2003, Dynamic calibration of force balances for impulse hypersonic facilities, Shock Waves., 12, 443, 10.1007/s00193-003-0181-6
Sahoo, 2005, Dynamic force balances for short-duration hypersonic testing facilities, Exp. Fluids., 38, 606, 10.1007/s00348-005-0932-5
K. Tanimizu, D. Mee, R. Stalker, Comparison of drag measurements of two axisymmetric scramjet models at Mach 6, In Proceedings of the 16th Australasian Fluid Mechanics Conference, 16AFMC. School of Engineering, The University of Queensland, 1299–1303 (2007).
Tanimizu, 2009, Drag force on quasi axisymmetric scramjets at various flight Mach numbers: theory and experiment, Shock Waves., 19, 83, 10.1007/s00193-009-0194-x
Boyce, 2007, Re-entry body drag: shock tunnel experiments and computational fluid dynamics calculations compared, Shock Waves., 16, 431, 10.1007/s00193-007-0086-x
Vadassery, 2013, Design and testing of an external drag balance for a hypersonic shock tunnel, Measurement., 46, 2110, 10.1016/j.measurement.2013.03.011
Nanda, 2017, Shock tube as an impulsive application device, Int. J. Aerospace Eng., 2017, 10.1155/2017/2010476
Sahoo, 2007, Design and analysis of a flat accelerometer-based force balance system for shock tunnel testing, Measurement., 40, 93, 10.1016/j.measurement.2006.03.016
Mahapatra, 2008, Effect of counterflow argon plasma jet on aerodynamic drag of a blunt body at hypersonic Mach numbers, Aeronaut. J., 112, 683, 10.1017/S0001924000590009
Saravanan, 2009, Aerodynamic force measurement using 3-component accelerometer force balance system in a hypersonic shock tunnel, Shock Waves., 18, 425, 10.1007/s00193-008-0172-8
Satheesh, 2009, Analysis of an internally mountable accelerometer balance system for use with non-isotropic models in shock tunnels, Measurement., 42, 856, 10.1016/j.measurement.2009.01.010
Kulkarni, 2010, Accelerometer-based force balance for high enthalpy facilities, J. Aerospace Eng., 23, 276, 10.1061/(ASCE)AS.1943-5525.0000040
Kulkarni, 2010, Counterflow drag reduction studies for a blunt cone in high enthalpy flow, Int J. Hypersonics., 1, 69, 10.1260/1759-3107.1.1.69
Balakalyani, 2019, An accelerometer balance for aerodynamic force measurements over Hypervelocity Ballistic models in shock tunnel, Measurement, 136, 636, 10.1016/j.measurement.2018.12.099
K. Kim, B. Jang, G. Park, Force Measurement Using an External Drag Balance in a Shock Tunnel, In23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2020.
Abdel-Jawad, 2007, New calibration technique for multiple-component stress wave force balances, Rev. Sci. Instrum., 78, 10.1063/1.2744235
Nanda, 2016, Design of artificial neuro-fuzzy based methodology for six component force balance, Procedia Eng., 144, 528, 10.1016/j.proeng.2016.05.038
Ramesh, 2018, Application of neural-networks and neuro-fuzzy systems for the prediction of short-duration forces acting on the blunt bodies, Soft Comput., 23, 5725, 10.1007/s00500-018-3231-9
Nanda, 2019, An innovative approach for prediction of aerodynamic coefficients in shock tunnel testing with soft computing techniques, Measurement., 134, 773, 10.1016/j.measurement.2018.11.007
Nanda, 2019, A comparison of accelerometer and piezofilm-based force balances for hypersonic shock tunnels, P. I. Mech. Eng. G-J. Aer., 233, 5310
Azari, 2014, Radial forging force prediction through MR, ANN, and ANFIS models, Neural Comput. Appl., 25, 849, 10.1007/s00521-014-1562-8