Ĭarter MB, Campbell RL, Pendergraft OC, Friedman DM, Serrano L (2006) Designing and testing a blended wing body with boundary-layer ingestion nacelles. Sgueglia A, Schmollgruber P, Benard E, Bartoli N, Morlier J (2018) Preliminary sizing of a medium range blended wing-body using a multidisciplinary design analysis approach. 41st Aerospace Sciences Meeting and Exhibit, 42(3). Ĭarlsson M (2003) Control surface response of a blended wing body aeroelastic wind tunnel model. Scholar A (2005) Experimental study of the subsonic aerodynamics of a blended wing body air vehicle with a focus on rapid technology assessmentĬarlsson M, Kuttenkeuler J (2003) Design and testing of a blended wing body aeroelastic wind-tunnel model. Collection of Technical Papers-AIAA Applied Aerodynamics Conference, 1(June), pp 217–234. Gebbie DA, Reeder MF, Tyler C, Fonov V, Crafton J (2005) PSP-based experimental investigation of a blended wing body aircraft. ![]() Mv M, Mondal P, Karn PK, Kumar P (2019) Numerical and experimental investigation of blended wing body configuration. Gebbie DA, Reeder MF, Tyler C, Fonov V, Crafton J (2007) Lift and drag characteristics of a blended-wing body aircraft. It is likely that the information acquired in this paper could be useful to the future BWB aircraft design and study along with its various geometric alterations and uses.Īngelo S, Potty V, Srinivasa Rao P, Srinivas G (2019) Aircraft fuselage recent developments-a review. The BWB is a new revolutionary concept that can find its way into the modern aircraft design, but it has certain limitations that need to be addressed before using this design commercially or in military aircraft. The studies done in implementing the advantages of BWB in UAVs and under water bodies are also mentioned in this review. This paper gives a holistic review of various experimental, numerical, and theoretical studies done on the topic along with the basic analysis and study along various recent developments like geometric alterations such as canard or gurney flaps. Due to these issues, this design cannot be used predominantly in the aircraft industry. ![]() The major two drawbacks of this design are the handling and the complex design. Due to this design, the aerodynamic performance of the aircraft is enhanced as a result there is reduction in noise and fuel consumption. ![]() Blended wing body (BWB) is a new design in which both the fuselage and the wings form the lifting surface of the body.
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