Results 91 to 100 of about 153 (119)

CFD based design optimization of dimples induced on Blended Wing Body airframe using the Taguchi method. [PDF]

PLoS One
Ali H, Rasani MR, Harun Z, Shahid MA.
europepmc   +1 more source

Deep-Sea Biomimetic Manta Ray Robots: A Comprehensive Review Based on Operational Depth Spectrum, Structures, Energy Optimization, and Control Systems. [PDF]

Biomimetics (Basel)
Ye L, Liu H, Ding Q, Hu Z, Li W, Cui W, Fan D.   +6 more
europepmc   +1 more source

Direct carbon dioxide emissions from civil aircraft. [PDF]

Atmos Environ (1994), 2014
Grote M, Williams I, Preston J.
europepmc   +1 more source

A review on aero-engine inlet-compressor integration and inlet flow distortion in axial compressors. [PDF]

Fundam Res
Li Z, Sun D, Dong X, Sun X.
europepmc   +1 more source

An efficient PanAir integrated framework for automated analysis. [PDF]

Sci Rep
Shahid T, Gürkan C.
europepmc   +1 more source

Analysis of crash response of a typical blended wing body aircraft under various emergency landing attitudes

Jixie qiangdu
ObjectiveIn order to investigate the structural response of a blended-wing-body aircraft under various emergency landing attitudes, a full-scale finite element model of the BWB aircraft was established, encompassing the main structural components of the ...
XIE Jiang, CHENG Siwuwei, HE Junlong, SHI Xiaopeng   +3 more
doaj  

Étude de la stabilité d'un avion BWB (Blended Wing Body) de 200 passagers

openaire   +1 more source

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Wind Tunnel experiments of UiTM's blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) at low subsonic speed

2010 International Conference on Science and Social Research (CSSR 2010), 2010
An experimental investigation is conducted to obtain aerodynamic characteristics and performance of a blended wing-body aircraft (BWB) under study by UiTM. The BWB design for unmanned aerial vehicle (UAV) known as “Baseline-II” is actually a completely-revised, redesigned version of “Baseline-I” BWB. The Baseline-II features have introduced a canard, a
Firdaus Mohamad, Rizal Nasir, Zurriati Mohd Ali   +2 more
exaly   +2 more sources

Experimental investigation of center elevator deflection on aerodynamics of UiTM's Baseline-I Blended Wing Body (BWB) unmanned aerial vehicle (UAV)

2010 International Conference on Science and Social Research (CSSR 2010), 2010
This paper describes the wind tunnel testing of a Blended Wing Body (BWB)-Baseline I with elevator developed in Universiti Teknologi MARA (UiTM). The experiment work was carried out in UiTM low speed wind tunnel using 1∶7 scaled model of BWB at Mach 0.1. The testing is conducted for center elevator angle between −10° to +10° until stall angle.
Rizal Nasir, Wahyu Kuntjoro, Wirachman Wisnoe   +2 more
exaly   +2 more sources