589
Views
1
CrossRef citations to date
0
Altmetric
Research Article

Inverse shape design method based on pressure and shear stress for separated flow via Elastic Surface Algorithm

, ORCID Icon & ORCID Icon
Pages 2357-2400 | Received 16 Apr 2020, Accepted 05 Apr 2021, Published online: 28 Apr 2021

References

  • Jahangirian A, Shahrokhi A. Inverse design of transonic airfoils using genetic algorithm and a new parametric shape method. Inverse Probl Sci Eng. 2009;17:681–699.
  • Matsushima K, Takanashi S. An inverse design method for wings using integral equations and Its Recent progress. In: K Fujii, GS Dulikravich, editors. Recent development of aerodynamic design methodologies: inverse design and optimization. Braunschweig/Wiesbaden: Springer Vieweg; 1999. p. 179–209.
  • Hajilouy-Benisi A, Nili-Ahmadabadi M, Durali M, et al. Duct design in subsonic and supersonic flow regimes with and without normal shock waves using flexible string algorithm. Scientia Iranica. 2010;17(3):179-193.
  • Dulikravich G, Baker D. Aerodynamic shape inverse design using a Fourier series method, in AIAA 99-0185; 1999.
  • Ashrafizadeh A, Raithby GD, Stubley GD. Direct design of airfoil shape with a prescribed surface pressure. Numer Heat Trans Part B: Fund. 2004;46(6):505–527.
  • Ashrafizadeh A, Raithby G. Direct design solution of the elliptic grid generation equations. Numer Heat Trans Part B: Fund. 2006;50(3):217–230.
  • Stanitz JD. Design of two-dimensional channels with prescribed velocity distributions along the channel walls, SEE NACA-TN-2593; NACA-TN-2595, 1952.
  • Stanitz JD. Aerodynamic design of efficient two-dimensional channels. Trans ASME. 1953;M. P. No. 52-A-110:1241–1255.
  • Stanitz JD. General design method for three-dimensional potential flow fields. NASA Contractor Report 3288; 1980.
  • Stanitz JD. A review of certain inverse methods for the design of ducts with 2- or 3-dimensional potential flow. Appl Mech Rev. 1988;41(6):217–238.
  • Zannetti L. A natural formulation for the solution of two-dimensional or axisymmetric inverse problems. Int J Numer Methods Eng. 1986;22(2):451–463.
  • Ashrafizadeh A, Alinia B, Mayeli P. A new co-located pressure-based discretization method for the numerical solution of incompressible Navier-Stokes equations. Numer Heat Trans Part B: Fund. 2015;67(6):563–589.
  • Nikfar M, Ashrafizadeh A. A coupled element-based finite-volume method for the solution of incompressible Navier-Stokes equations. Numer Heat Trans Part B: Fund. 2016;69(5):447–472.
  • Nili-Ahmadabadi M, Durali M, Hajilouy-Benisi A, et al. Inverse design of 2-D subsonic ducts using flexible string algorithm. Inverse Probl Sci Eng. 2009;17(8):1037–1057.
  • Nili-Ahmadabadi M, Hajilouy-Benisi A, Ghadak F, et al. A novel 2D incompressible viscous inverse design method for internal flows using flexible string algorithm. J Fluids Eng. 2010;132(3):031401.
  • Madadi A. 3D-dimensional ball-spine algorithm for determining the profile of an axial flow compressor with specified pressure distribution [PhD thesis]. Mechanical Engineering, Amir Kabir University of Technology; 2014.
  • Dulikravich G. Aerodynamic shape design and optimization: status and trends. AIAA J Aircraft. 1992;29(5):1020–1026.
  • Dulikravich G. Shape inverse design and optimization for three-dimensional aerodynamics. AIAA invited paper 95-0695, AIAA aerospace sciences meeting, Reno, NV; 1995.
  • Dulikravich G. Design and optimization tools development, chapters no. 10–15. In: H Sobieczky, editor. New design concepts for high speed air transport. Wien/New York: Springer; 1997. p. 159–236.
  • Garabedian P, McFadden G. Computational fluid dynamics of airfoils and wings. In: RE Meyer, editor. Transonic, shock, and multidimensional flows. New York: Academic Press; 1982. p. 1–16.
  • Garabedian P, McFadden G. Design of supercritical swept wings. AIAA J. 1982;20(3):289–291.
  • Malone J, Sankar L, Vadyak J. Inverse aerodynamic design method for aircraft components. J Aircr. 1987;24:8–9.
  • Malone J, Vadyak J, Sankar L. A technique for the inverse aerodynamic design of nacelles and wing configurations. AIAA Pap.1985;AIAA-85-4096:1-9 .
  • Malone J, Narramore J, Sankar L. Airfoil design method using the Navier-Stokes equations. J Aircr. 1991;28(3):216–224.
  • Dulikravich G, Baker DP.. Fourier series analytical solution for inverse design of aerodynamic shapes. In: Tanaka M, Dulikravich GS, editors. Inverse problems in mechanics (ISIP '98). Nagano City, Japan: Elsevier Science, Ltd.; 1998. p. 427–436.
  • Thinsurat K. Inverse design of airfoils using a flexible membrane method [Master thesis]. University of Texas at Arlington; 2010.
  • Dulikravich GS, Baker DP. Using existing flow-field analysis codes for inverse design of three-dimensional aerodynamic shapes. In: K Fujii, GS Dulikravich, editor. Recent development of aerodynamic design methodologies: inverse design and optimization. Wiesbaden: Vieweg + Teubner Verlag; 1999. p. 89–112.
  • Hazarika N. An efficient inverse method for the design of blended wing-body configurations [PhD thesis]. Georgia Institute of Technology; 1989.
  • Teck W, And T, Zangeneh M. A novel 3D inverse method for the design of turbomachinery blades in rotational viscous flow: theory and applications. Task Quart J. 2002;6(1):63–78.
  • Rahmati MT. A new Navier-Stokes inverse method based on mass-averaged tangential velocity for blade design. Int J Numer Methods Fluids. 2009;60(3):323–336.
  • Nili-Ahmadabadi M, Hajilouy-Benisi A, Durali M, et al. Duct design in subsonic and supersonic flow regimes with and without normal shock wave using flexible string algorithm. Proc ASME Turbo Expo. 2009;7(48883):513–523.
  • Nili-Ahmadabadi M, Durali M, Hajilouy A. A novel aerodynamic design method for centrifugal compressor impeller. J Appl Fluid Mech. 2014;7(2):329–344.
  • Nili Ahmadabadi M, Poursadegh F. Centrifugal compressor shape modification using a proposed inverse design method. J Mech Sci Technol. 2013;27:713–720.
  • Shumal M, Nili-Ahmadabadi M, Shirani E. Development of the ball-spine inverse design algorithm to swirling viscous flow for performance improvement of an axisymmetric bend duct. Aerosp Sci Technol. 2016;52:181–188.
  • Poursadegh F, Hajilouy-Benisi A, Nili-Ahmadabadi M. A novel quasi-3D design method for centrifugal compressor impeller on the blade-to-blade plane. Proc ASME Turbo Expo 2010: Power for Land, Sea, and Air. 2011;54679:1155–1162.
  • Nili-Ahmadabadi M, Poursadegh F. Centrifugal compressor shape modification using a proposed inverse design method. J Mech Sci Technol. 2013;27(3):713–720.
  • Nili-Ahmadabadi M, Ghadak F, Mohammadi M. Subsonic and transonic airfoil inverse design via ball-spine algorithm. Comput Fluids. 2013;84:87–96.
  • Madadi A, Kermani MJ, Nili-Ahmadabadi M. Aerodynamic design of S-shaped diffusers using ball–spine inverse design method. J Eng Gas Turbine Power. 2014;136(12):122606–122606-8.
  • Madadi A, Kermani MJ, Nili-Ahmadabadi M. Applying the ball-spine algorithm to the design of blunt leading edge airfoils for axial flow compressors. J Mech Sci Technol. 2014;28(11):4517–4526.
  • Madadi A, Kermani MJ, Nili-Ahmadabadi M. Application of the ball-spine algorithm to design axial-flow compressor blade. Scientia Iranica. 2014;21(6):1981–1992.
  • Madadi A, Kermani MJ, Nili-Ahmadabadi M. Application of an inverse design method to meet a target pressure in axial-flow compressors. Proc ASME Turbo Expo 2011: Power for Land, Sea, and Air. 2011;54679:1315–1322.
  • Madadi A, Kermani MJ, Nili-Ahmadabadi M. Three-dimensional design of axial flow compressor blades using the ball-spine algorithm. J Appl Fluid Mech. 2015;8(4):683–691.
  • Mayeli P, Nili-Ahmadabadi M, Besharati-Foumani H. Inverse shape design for heat conduction problems via the ball spine algorithm. Numer Heat Trans Part B: Fund. 2016;69(3):249–269.
  • Safari M, Nili-Ahmadabadi M, Ghaei A, et al. Inverse design in subsonic and transonic external flow regimes using Elastic Surface Algorithm. Comput Fluids. 2014;102:41–51.
  • Nasrazadani SH, Nili-Ahmadabadi M, Noorsalehi MH. Upgrade and development of elastic surface inverse design method for axial compressor cascade with sharp-edged blades. Numer Heat Transf. 2020;77(1):64–86.
  • Noorsalehi MH, Nili-Ahmadabadi M, Shirani E. Inverse design of axial-flow compressor blades using elastic surface algorithm in subsonic and transonic flow regimes with separation. Proc ASME Turbo Expo. 2016;GT2016-56717:1-14.
  • Felippa C. Nonlinear finite element methods, (ASEN 6107) DAES. Berlin, Heidelberg: Springer-Verlag / Boulder: University of Colorado;2012.
  • Ladson CL. Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 Airfoil Section, NASA TM 4074; 1988.
  • Eftekhari S, Al-Obaidi ASM. Investigation of a NACA0012 finite wing aerodynamics at low Reynolds numbers and 0° to 90° angle of attack. J Aerospace Technol Manage. 2019;11:1-11.
  • White FM. Viscous fluid flow, 3rd ed., international edition, University of Rhode Island, New York: McGraw-Hill; 2006.
  • Ghadimi P, Bakhshandeh Rostami A, Jafarkazemi F. Aerodynamic analysis of the boundary layer region of symmetric airfoils at ground proximity. Aerosp Sci Technol. 2012;17(1):7–20.
  • Yayun S, Junqiang B, Jun H, et al. Numerical analysis and optimization of boundary layer suction on airfoils. Chin J Aeronaut. 2015;28(2):357–367.

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.