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Aerodynamic Design and Exploration of a Blended Wing Body Aircraft at Subsonic Speed

<p>Blended Wing Body (BWB) is a novel aircraft concept which provides many different aerodynamic benefits over conventional aircrafts design. This research investigated the BWB design, L/D characteristics, surface pressure distribution and span-wise lift distribution of a BWB aircraft at low to medi...

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Hlavní autoři: Sam Dakka, Oliver Johnson
Médium: Artigo
Jazyk:Inglês
Vydáno: Embry-Riddle Aeronautical University 2019-01-01
Edice:International Journal of Aviation, Aeronautics, and Aerospace
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On-line přístup:https://commons.erau.edu/ijaaa/vol6/iss5/17
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