Aerodynamic design challenges of the blended-wing-body subsonic transport

18th Applied Aerodynamics Conference

Volumn , Issue , 2000, Pages

  Roman, D ^a   Allen, J B ^a   Liebeck, R H ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894450491     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Liebeck, R. EL, "Design of Subsonic Airfoils for High Lift", AIAA Journal of Aircraft, September 1978.
2. Liebeck, R. H., Page, M. A., Rawdon, B. K., Scott, P. W. and Wright, P. A., "Concepts for Advanced Subsonic Transports", NASA Contractor Report 4624, September 1994.
3. Liebeck, R. H., Page, M. A. and Rawdon, B. K, "Blended-Wing-Body Subsonic Commercial Transport", AIAA-98-0438, January 1998.
4. http://fmad-www.larc.nasa.gov:80/~biedron/ Cfl3dv6/cfl3dv6_home.htrnl#general
5. Pelkman, R. A., "Key Findings and Conclusions from an NTF Wind Tunnel Test of an Initial Blended-Wing-Body Concept", NASA Contract NAS1-20268, Boeing Report No. CRAD-9402- TR-3985, August 1998.
6. http://hpcc.arc.nasa.gov/insights/vol5/overflow.htm
7. Campbell, R. L., "Efficient Viscous Design of Realistic Aircraft Configurations", AIAA-98-2539, June 1998.
8. Jameson, A., "Re-Engineering the Design Process through Computation", AIAA-97-0641, January 1997.