Extensive supersonic natural laminar flow on the aerion business jet

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 12, Issue , 2007, Pages 8465-8481

  Sturdza, Peter ^a,b  

^a Desktop Aeronatutics Inc   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

JET AIRCRAFT; OPTIMIZATION; REYNOLDS NUMBER; SUPERSONIC FLOW;

AERION BUSINESS JET; AERODYNAMIC DESIGN; REVOLUTIONARY JET; SUPERSONIC NATURAL LAMINAR FLOW;

LAMINAR FLOW;

EID: 34250900363     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-685     Document Type: Conference Paper

References (23)

1. U.S. Patent No. 5322242, June 21, 1994, Richard R. Tracy, Carson City, NV.
2. Sakata, K., "Supersonic Experimental Airplane (NEXST) for Next Generation SST Technology," AIAA paper 2002-0527, Jan. 2002.
3. Ashill, P. R., and Smith, P. D., "An Integral Method for Calculating the Effects on Turbulent Boundary-Layer Development of Sweep and Taper," Aeronautical Journal, Vol. 89, Feb. 1985, pp. 43-54.
4. Bradshaw, P., Mizner, G. A., and Unsworth, K., "Calculation of Compressible Turbulent Boundary Layers on Straight-Tapered Swept Wings," AIAA Journal, Vol. 14, Mar. 1976, pp. 399-400.
5. Kaups, K, and Cebeci, T., "Compressible Laminar Boundary Layers with Suction on Swept and Tapered Wings," Journal of Aircraft, Vol. 14, Jul. 1977, pp. 661-667.
6. Horton, H. P., and Stock, H. W., "Computation of Compressible, Laminar Boundary Layers on Swept, Tapered Wings," Journal of Aircraft, Vol. 32, 1995, pp. 1402-1405.
7. Sturdza, P., Manning, V. M., Kroo, I., Tracy, R., "Boundary Layer Calculations for Preliminary Design of Wings in Supersonic Flow," AIAA Paper No. 99-3104, 28 Jun. 1999.
8. Kroo, I. M. and Sturdza, P., "Design-Oriented Aerodynamic Analysis for Supersonic Laminar Flow Wings," AIAA paper 2003-0774, Jan. 2003.
9. Sturdza, P., An Aerodynamic Design Method for Natural Laminar Flow Aircraft, Ph.D. Dissertation, Stanford University, Dec, 2003.
10. Dagenhart, J. R., "Amplified Crossflow Disturbances in the Laminar Boundary Layer on Swept Wings with Suction," NASA TP 1902, Nov. 1981.
11. Drela, M., "Two-Dimensional Transonic Aerodynamic Design and Analysis Using the Euler Equations," Ph.D. Dissertation, MIT GTL Rept. No. 187, Feb. 1986.
12. Gleyzes, G., Cousteix, J., and Bonnet, J. L., "A Calculation Method of Leading-Edge Separation Bubbles," in Numerical and Physical Aspects of Aerodynamic Turbulent Flows II, edited by T. Cebeci, Springer-Verlag, New York 1984.
13. n Method for Transition Prediction in Two-Dimensional, Incompressible Boundary Layers," Z. Flugwiss. Weltraumforschung, Vol. 12, 1989, pp. 16-30.
14. Arnal, D., "Boundary Layer Transition: Predictions Based on Linear Theory," in Special Course on Progress in Transition Modeling, AGARD Rept. 793, Apr, 1994, pp. 2-1 to 2-63.
15. Rodriguez, D. L. and Sturdza, P., "A Rapid Geometry Engine for Preliminary Aircraft Design," AIAA paper 2006-929, Jan. 2006.
16. Derbyshire, T., and Sidwell, K. W., "PAN AIR Summary Document, (Version 1.0)," NASA CF-3250, 1982.
17. Aftosmis, M. J., Berger, M. J., Adomavicius, G., "A Parallel Multilevel Method for Adaptively Refined Cartesian Grids with Embedded Boundaries," AIAA-2000-0808, Jan. 2000.
18. Rodriguez, D. L., "Propulsion/Airframe Integration and Optimization on a Supersonic Business Jet," AIAA-2007-1048, Jan. 2007.
19. Nelder, J. A., Mead, R., "A Simplex Method for Function Minimization," Computer Journal, Vol 7, 1965, pp. 308-313.
20. Malik, M. R., "COSAL - A Black Box Compressible Stability Analysis Code for Transition Prediction in Three-Dimensional Boundary Layers," NASA CR-165925, May 1982.
21. Chang, C.-L., "The Langley Stability and Transition Analysis Code (LASTRAC) Version 1.2 User Manual," NASA TM-2004-213233, June 2004.
22. McTigue, J. G., Overton, J. D., and Petty, G., Jr., "Two Techniques for Detecting Boundary-Layer Transition in Flight at Supersonic Speeds and at Altitudes Above 20,000 Feet," NASA TN D-18, 1959.
23. Banks, D. W., Van Dam, C. P., Shui, H. J., and Miller, G. M., "Visualization of In-Flight Flow Phenomena Using Infrared Thermography," 9th International Symposium on Flow Visualization, Edinburgh, UK, 2000.