Abstract
Two new methods are presented for solving the Euler equations using a compact higher order polynomial reconstruction technique on unstructured grids. The methods use a characteristic-based approach with a cell-centered finite volume method. For transonic Ringleb flow, computations are performed for first order to fourth order accuracy and are compared with the hodograph solution. Results for a 10 degree ramp case are also presented. An analysis is performed which demonstrates that the higher order method is an order of magnitude more efficient than the lower order method in modeling the flow for moderate to fine error tolerances. Accuracy, speed and memory requirements are evaluated in the efficiency study.
Original language | English |
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DOIs | |
State | Published - 1991 |
Event | 9th Applied Aerodynamics Conference, 1991 - Baltimore, United States Duration: Sep 23 1991 → Sep 25 1991 |
Conference
Conference | 9th Applied Aerodynamics Conference, 1991 |
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Country/Territory | United States |
City | Baltimore |
Period | 09/23/91 → 09/25/91 |