flapping wing造句
例句與造句
- Flexibility of flapping wing and its effect on aerodynamic characteristic
撲翼柔性及其對氣動特性的影響 - Attitude tracking control for flapping wing micro aerial vehicle based on feedback compensation
基于反饋補償?shù)膿湟砦⑿惋w行器姿態(tài)跟蹤控制 - In fine , as long as effort will include results , as long as pay will have repay , as long as give me a terrace for displaying , i can flap wings to rise high fly
總之，只要努力就會有收獲，只要付出就會有回報，只要給我一個施展的平臺，我就能振翅高飛！ - 2 . the 3 - d unsteady euler equations are derived . and the computational program based on these equations is developed to adapt for the calculations of flapping wing
2 、推導(dǎo)了非定常情況下的三維歐拉方程，發(fā)展了三維非定常歐拉方程計算程序，使之適應(yīng)于撲動翼計算的需要。 - Applying this dissertation , the aerodynamic characteristics of flapping wing can be calculated , the effects of every factor can be analyzed and some qualitative instructions can be given
運用本文可以計算撲翼的氣動特性及分析各參數(shù)對撲翼氣動特性的影響，進(jìn)而指導(dǎo)撲動翼微型飛機的初期設(shè)計。 - It's difficult to find flapping wing in a sentence. 用flapping wing造句挺難的
- 5 . effects of unsteady flows on the aerodynamic characteristics are also analyzed . the results of this dissertation are useful for the further investigations of three - dimensional flapping wing
對于非定常不可壓流動，分析了運動參數(shù)對翼型氣動特性的影響，為進(jìn)一步研究繞三維撲翼的非定常流動打下基礎(chǔ)。 - Aimed at the mechnical flapping wing system of the bionicflying micro - robot including the micro - actuators , the bionic wing , the locomotion system , and the energy source , the scaling effect is analyzed
針對微型仿生撲冀飛行器的機械撲冀系統(tǒng)，包括微驅(qū)動器、仿生翅、運動系統(tǒng)和動力源等，本文進(jìn)行了尺度效應(yīng)分析。 - 3 . the effects of every flapping control parameters on the aerodynamic characteristics of flapping wing are investigated . its results lay a foundation for the further investigations of flapping wing micro air vehicles
3 、研究了運動各參數(shù)對撲翼的氣動特性的影響，為撲翼微型飛機的進(jìn)一步研究設(shè)計打下了基礎(chǔ)。 - Combined with blade element theory , the results can be used to evaluate aerodynamic characteristics of flapping wings , which are helpful for the initial design of micro rotary and flapping wing
運用本文方法分析了各參數(shù)對翼型氣動特性的影響，進(jìn)一步結(jié)合葉素理論還可以估算撲翼的氣動特性，進(jìn)而指導(dǎo)微旋翼或撲翼微型飛行器的初期設(shè)計。 - The main aspects of this dissertation are as follows : 1 . employing the moving grid technique , a 3 - d moving grid based on the transfinite interpolation is developed . this grid has better adaptation than the deforming grid for flapping wing
本文的主要工作表現(xiàn)在以下幾個方面： 1 、引入運動網(wǎng)格技術(shù)，發(fā)展了一套基于廣義無限插值理論的適合撲翼計算的三維運動網(wǎng)格，提高了網(wǎng)格對撲動機翼的適應(yīng)性。 - Results show that the bionic flying can be more easily realized when the scaling sizes are decreased , thus making high flapping frequency motion by the resonance , and meeting the power needs of the flapping wing for the electrostatic , the electromagnetic and piezoelectric actuators
分析結(jié)果表明，當(dāng)尺寸減小時，仿生飛行更容易實現(xiàn)：通過共振能實現(xiàn)高頻運動，微靜電、電磁和壓電驅(qū)動器都能滿足撲翼系統(tǒng)功率需求。 - The flapping wing system of a bionic flying micro - robot based on insects and birds aggregates the lift , hovering and push functions , its kinematics and aerodynamics are different from that of fixed wing and rotational wing , and so bionic flying micro - robot must be studied from bionics initially
摘要模仿昆蟲和小鳥飛行的撲翼飛行機器人將舉升、懸停和推進(jìn)功能集于一個撲翼系統(tǒng)，與固定翼和旋翼完全不同，因此研究只能從生物仿生開始。 - In this thesis , finite volume method and dual - time stepping method are employed to solve the 3 - d unsteady euler equations . the unsteady flow field around a finite - span flapping wing is simulated . the lift and thrust of the flapping wing for different cases are calculated
本文運用有限體積法結(jié)合雙時間推進(jìn)技術(shù)求解三維非定常歐拉方程，模擬了有限翼展機翼在同時具有上下拍動和俯仰運動狀態(tài)下的非定常流場，計算了不同狀態(tài)下?lián)湟淼纳巴屏?，分析了各個影響因素對撲翼氣動特性的影響。