This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Computational Support to Engine Test
Annotation ability available
Sector:
Language:
English
Abstract
The rapid development and improvement of computational simulation analysis codes coupled with improved performance of modern computers, increases the scope of fluid dynamics, structural, and heat-transfer problems which can be addressed. At the same time, propulsion systems have become increasingly complex as mission criteria push the limits of present technologies. These propulsion system advancements require detailed understanding of engine performance and test cell interactions. Accordingly computational simulation capability is growing into a role which complements and enhances many phases of engine system design, including test and evaluation. At the Arnold Engineering Development Center (AEDC) computational analyses have become an integral part of the hardware testing process by providing information for pretest facility design; instrumentation; and posttest analysis to reduce risks and improve test facility capabilities.
Recommended Content
Aerospace Standard | Measurement Uncertainty Applied to Cost-Effective Testing |
Aerospace Standard | Advanced Ducted Propulsor In-Flight Thrust Determination |
Authors
Citation
PRUFERT, M., McCLURE, M., and POWER, G., "Computational Support to Engine Test," SAE Technical Paper 942141, 1994, https://doi.org/10.4271/942141.Also In
References
- Steinbrenner J. P. Chawner J. R. Anderson D. A. “Enhancement to the GRIDGEN System for Increased User Efficiency and Grid Quality.” AIAA-92-0662 30th Aerospace Sciences Meeting Reno, NV January 1992
- Cooper, G. K. Sirbaugh, J. R. “PARC Code: Theory and Usage.” December 1989
- Pinker, R. A. Herbert, M. V. “Pressure Loss Associated with Compressible Flow Through Square-Mesh Wire Gauzes.” Journal of Mechanical Engineering Science 9 1 1967 11 23
- Tucker, M. “Approximate Calculation of Turbulent Boundary-Layer Development in Compressible Flow.” April 1951
- Hodge, B. K. Adams, J. C., Jr. “The Calculation of Compressible Transitional, Turbulent, and Relaminarization Boundary Layers over Smooth and Rough Surfaces using an Extended Mixing Length Hypothesis.” February 1978
- Cooper G. K. Phares W. J. “CFD applications in an Aerospace Engine Test Facility.” AIAA Paper No. 90-2003 AIAA/ASME/SAE/ASEE 26th Joint Propulsion Conference Orlando, FL July 1990
- Pulliam, T. H. Steger, J. L. “Euler and Thin Layer Navier-Stokes Codes: ARC2D, ARC3D.” Computational Fluid Dynamics University of Tennessee Space Institute Tullahoma, TN UTSI Publication E02-40905-023-84 March 12-16 1984 15.1 15.85
- Roberts, J. H. Guidone, J. A. Mancuso, B. Babilon, J. McIlveen, M. “Engine Testing at Simulated Altitiude Conditions” AIAA Paper No. 93-2452 AIAA/ASME/SAE/ASEE 29th Joint Propulsion Conference and Exhibit Monterey, CA
- Power, G. D. Heikkinen, B. D. “CFD Applications in an Aeropropulsion Test Environment.” AIAA Paper No. 93-1924 AIAA/ASME/SAE/ASEE 29th Joint Propulsion Conference and Exhibit Monterey, CA
- Savelle, S. A. Prufert, M. B. “Turbine Engine Performance Test and Evaluation Techniques.” AIAA Paper No. 92-3977 AIAA 17th Aerospace Ground Testing Conference Nashville, TN