Results 21 to 30 of about 2,668 (117)

Comprehensive strategy of sonodynamic therapy and gas therapy on tumor treatment. [PDF]

Med Gas Res
Zhao L, Zhang Y, Huang Q, Zhang T.
europepmc   +1 more source

Butterfly Clap-Fling Flight Mechanisms Observed by Schlieren Imaging for the Design of Bio-Inspired Micro Air Vehicles. [PDF]

Biomimetics (Basel)
Prisăcariu EG, Strătilă S, Dumitrescu O, Sima M, Roșu RA, Vlăducă I.   +5 more
europepmc   +1 more source

Numerical Study into the Spanwise Effects for the Three-Dimensional Unsteady Flow over a Bio-Inspired Corrugated Infinite Wing at Low Reynolds Number. [PDF]

Biomimetics (Basel)
Alhinai A, Schenkel T.
europepmc   +1 more source

CFD-driven neural network and SVM models for airfoil aerodynamic enhancement with bio-inspired riblets and plasma actuation. [PDF]

Sci Rep
Karthikeyan KV, Raju A, Jain J, Lekshmanan S, Rajan H.   +4 more
europepmc   +1 more source

Enhanced aerodynamic and mechanical performance of double-rotor wind turbines via a one-way fluid-structure interaction analysis. [PDF]

PLoS One
Yang Y, Zhuang W, Yuan P, Yuan R, Yuan J, Sun F, Hu Y.   +6 more
europepmc   +1 more source

Bridging spatial and temporal surface pressure dynamics for gust aerodynamic modeling. [PDF]

Commun Eng
Chen D, Liang A, Sun B, Rival DE, Fan D.
europepmc   +1 more source

Improved positioning criterion and imaging scheme of deep UV planar laser-induced fluorescence technology. [PDF]

iScience
Wu H, Dai S, Zhang Z, Huang H, Wu L, Lin W.   +5 more
europepmc   +1 more source

Dynamic Wear Modeling and Experimental Verification of Guide Cone in Passive Compliant Connectors Based on the Archard Model. [PDF]

Polymers (Basel)
He Y, Wang B, Zhao F, Hong X, Fang L, Xu W, Liao M, Tian F.   +7 more
europepmc   +1 more source

Kinematic and aerodynamic modeling of flexible wings with wing root adjustment for flapping wing micro aerial vehicles. [PDF]

Sci Rep
Liu Z, Zhang X, Wang Z, Ye R.
europepmc   +1 more source

Aerodynamic design of supersonic experimental airplane

Aerodynamic design of supersonic experimental airplane
航空宇宙技術研究所 17-19 Jan. 2000 東京 日本 National Aerospace Laboratory 17-19 Jan. 2000 Tokyo Japan 超音速輸送機に対するNALの実験(NEXST(小型超音速実験機計画)-1)の第1段階において、超音速航行時での抵抗軽減のための空力設計に焦点が当てられた。CFD(計算流体力学)が、この研究には大変有益であると考えられた。設計段階で4つの空力概念が適用された。(1)矢羽根平面型、(2)ねじれ翼、(3)面積則胴体、(4)自然層流(NLF)翼である。NLFの概念は摩擦抵抗低減のために考案された。NLFは今までSSTに適用されたことはなく、このプロジェクト独自の試みである。NLFを実現するために、先ず ...
openaire