A multidisciplinary optimization method for designing boundary layer ingesting inlets

9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 2002, Pages

  Rodriguez, David L ^a  

^a STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; AIRCRAFT PROPULSION; DESIGN; ENGINES; NAVIER STOKES EQUATIONS;

ANALYSIS METHOD; BLENDED WING BODY; COMPLEX VARIABLE METHOD; CONCEPTUAL AIRCRAFT DESIGNS; DESIGN INTEGRATIONS; MULTI-DISCIPLINARY OPTIMIZATIONS; NAVIER-STOKES FLOW SOLVER; PROPULSION SYSTEM;

OPTIMIZATION;

EID: 34147105104     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Smith, L.H., "Wake Ingestion Propulsion Benefit," Journal of Propulsion and Power, Vol. 9, No. 1, pp. 74-82.
2. Rodriguez, D.L. and Kroo, I.M., "A 2D Multidisciplinary Design Method for Boundary Layer Ingesting Inlets," AIAA 99-0838, 1999.
3. Rodriguez, D.L., "A 3D Multidisciplinary Design Method for Boundary Layer Ingesting Inlets," AIAA 2000-0424, 2000.
4. Rodriguez, D.L., "A Multidisciplinary Optimization Method for Designing Inlets Using Complex Variables," AIAA 2000-4875, 2000.
5. Rumsey, C., Sanetrik, M., Biedron, R., Melson, N., and Parlette, E., "Efficiency and Accuracy of Time-Accurate Turbulent Navier-Stokes Computations," Computers & Fluids, Vol. 25, No. 2, pp. 217-236, 1996.
6. Spalart, P. and Allmaras, S., "A One-Equation Turbulence Model for Aerodynamic Flows," AIAA 92-0439, 1992.
7. Klann, J. and Snyder, C., NEPP Programmer's Manual, NASA TM 106575, 1994.
8. Gill, P.E., Murray, W., Saunders, M.A., Wright, M.H., "User's Guide For NPSOL 5.0: A Fortran Package for Nonlinear Programming," TR SOL 94, Stanford University, 1994.
9. Jameson, A., "Aerodynamic Design Via Control Theory," NASA CR-181749, 1988.