The primary motivation behind the paper is to think about the streamlined and steadiness attributes of a mixed wing-body (BWB) air ship. This paper exhibits the estimation and determination of air ship outline parameters, plan form plan, reflex airfoils, and behaviour intensive dependability examination of the flying machine. A calculated configuration of BWB flying machine has been done and the outline was broke down and refined to accomplish static security. The CFD examination of the BWB air ship was done at three distinct estimations of approach (AOA) and subsequently the slow down AOA was resolved from the computational results. The dynamic solidness of the flying machine has been studied under five modes in particular brief period, phugoid, Dutch-move, roll and winding. The static dependability has been accomplished with a wide positive estimation of static edge. Comes about additionally demonstrate that the flying machine is powerfully steady for longitudinal and horizontal modes when subjected to aggravations in separate conditions. The BWB flying machine satisfies the criteria of Class I Category B airplane and shows flight level 1 qualities in all security modes.

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Bullard, D. (1997-2008). Horten Biography. Retrieved October 2015, from Douglas Bullard Website: n_Biography/horten_biography.html

NASA. (2015). NASA Website. Retrieved August 2015, from _wing_tests.html

Liebeck, R. H., Page, M. A., & Rawdon, B. K. (1998). Blended Wing Body Subsonic Commercial Transport. AIAA Paper 98-0438.

Qin, N., Vavelle, A., Le Moigne, A., Hackett, K., &Weinerfelt, P. (2002). Aerodynamic Studies for Blended Wing Body Aircraft. AIAA.

Roman, D., Gilmore, R., & Wakayama, S. (2003). Aerodynamics of High-subsonic Blended Wing Body Configuration. AIAA Paper.

Qin, N., &Weinerfelt, P. (2004). Aerodynamic Considerations of Blended Wing Body Aircraft. Progess in Aerospace Sciences, 40, 321-343.


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