| Type of Document |
Dissertation |
| Author |
Lindau, Jules Washington
|
| URN |
etd-02132009-171914 |
| Title |
Multidimensional dynamic compression system modeling |
| Degree |
PhD |
| Department |
Mechanical Engineering |
| Advisory Committee |
| Advisor Name |
Title |
| O'Brien, Walter F. |
Committee Chair |
| Davis, Milton W. Jr. |
Committee Member |
| Moore, John |
Committee Member |
| Ng, Wing F. |
Committee Member |
| Walters, Robert W. |
Committee Member |
|
| Keywords |
- two-dimensional post-stall model
|
| Date of Defense |
1995-06-05 |
| Availability |
restricted |
Abstract
A more robust method for solving the governing equations of a one-dimensional stage-by-stage dynamic compression system model was developed and validated. The improved
method was then applied to two-dimensional post-stall models. The improvement in robustness
was achieved by modeling the governing equations with upwind differencing and use of implicit
time integration. A special form of upwind flux, flux difference splitting with source term
treatment, FDSS, was developed for the model. A two-dimensional axisymmetric model was
developed to allow post-stall modeling of split flowpath systems such as turbofans. This model
was an entirely new concept. Additionally, a two-dimensional axial-circumferential model of
rotating stall cell development and propagation was developed based on previous work. All of
the models developed applied upwind differencing techniques to improve upon central-difference
methods.
|
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