| contributor author | H. U. Akay | |
| contributor author | A. Ecer | |
| date accessioned | 2017-05-08T23:10:58Z | |
| date available | 2017-05-08T23:10:58Z | |
| date copyright | October, 1981 | |
| date issued | 1981 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26769#657_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/94468 | |
| description abstract | Analysis of transonic flow through a cascade of airfoils is investigated using the finite element method. Development of a computational grid suitable for complex flow structures and different types of boundary conditions is presented. An efficient pseudo-time integration scheme is developed for the solution of equations. Modeling of the shock and the convergence characteristics of the developed scheme are discussed. Numerical results include a 45 deg staggered cascade of NACA 0012 airfoils with inlet flow Mach number of 0.8 and angles of attack 1, 0, and −1 deg. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Transonic Flow Computations in Cascades Using Finite Element Method | |
| type | Journal Paper | |
| journal volume | 103 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3230788 | |
| journal fristpage | 657 | |
| journal lastpage | 664 | |
| identifier eissn | 0742-4795 | |
| keywords | Finite element methods | |
| keywords | Computation | |
| keywords | Transonic flow | |
| keywords | Airfoils | |
| keywords | Cascades (Fluid dynamics) | |
| keywords | Flow (Dynamics) | |
| keywords | Mach number | |
| keywords | Equations | |
| keywords | Shock (Mechanics) | |
| keywords | Modeling AND Boundary-value problems | |
| tree | Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 004 | |
| contenttype | Fulltext | |
