A 2D multidisciplinary design method for boundary layer ingesting inlets

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Rodriguez, David L ^a   Kroo, Ilan M ^a  

^a STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; ENGINES; NAVIER STOKES EQUATIONS; NONLINEAR PROGRAMMING; PROPULSION;

BLENDED WING BODY; CONCEPTUAL AIRCRAFT DESIGNS; DESIGN INTEGRATIONS; LOW-MOMENTUM FLOWS; MULTI-DISCIPLINARY DESIGNS; MULTI-DISCIPLINARY OPTIMIZATIONS; NAVIER-STOKES FLOW SOLVER; PROPULSIVE EFFICIENCIES;

DESIGN;

EID: 84983143284     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-838     Document Type: Conference Paper

References (6)

1. Smith, L.H., "Wake Ingestion Propulsion Benefit" Journal of Propulsion and Power, Vol. 9, No. 1, pp. 74-82.
2. Swanson, R.C., and Turkel, E., "A Multistage Time-Stepping Scheme for the Navier-Stokes Equations" AIAA 85-0035, 1985.
3. Spalart, R and Allmaras, S., "A One-Equation Turbulence Model for Aerodynamic Flows" AIAA 92-0439, 1992.
4. Klann, J. and Snyder, C, NEPP Programmer's Manual, NASA TM 106575, 1994.
5. 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.
6. Livesey, J.L., "Flow Property Averaging Methods for Compressible Internal Hows" AIAA 82-0135, 1982.