TY  - CONF

T1  - A study of spanwise lift distribution for blended wing body aircraft

JO  - CEAS Aerospace Aerodynamics Research Conference

PY  - 2003/06/01

AU  - Qin N

AU  - Vavalle A

AU  - Le Moigne A

ED  - 

SN  - 9781857681284

Y2  - 2024/12/26

ER  -