Titlebook: Aerodynamics of Tandem Wing Aircraft; From Dinosaurs to UA Illia S. Kryvokhatko Book 2025Latest edition The Editor(s) (if applicable) and T

只看該作者 · 發(fā)表于 2025-3-25 06:37:17

Recommendations Regarding Aerodynamic Design of Tandem Wing Aircraft,t is better to consider the conventional scheme, or canard, or flying wing). Then, how to choose the overall layout and dimensions of the tandem wing aircraft as the design process differs greatly from the one for a classical aircraft. Next, principal suggestions are listed if there is a need to (1)

只看該作者 · 發(fā)表于 2025-3-25 09:42:29

Determination of Tandem Wing Aircraft Aerodynamic Characteristics,cription of a wind tunnel model of a UAV with which multiple tests (weight and visual) were performed. Finally, the comparison of predictions by all the methods is presented including control surface effectiveness with wing-wing interference.

只看該作者 · 發(fā)表于 2025-3-25 15:35:56

只看該作者 · 發(fā)表于 2025-3-25 19:40:57

只看該作者 · 發(fā)表于 2025-3-25 21:15:43

7樓

只看該作者 · 發(fā)表于 2025-3-26 02:20:47

8樓

只看該作者 · 發(fā)表于 2025-3-26 08:18:39

8樓

只看該作者 · 發(fā)表于 2025-3-26 09:32:51

8樓

只看該作者 · 發(fā)表于 2025-3-26 14:09:28

9樓

只看該作者 · 發(fā)表于 2025-3-26 19:41:19

9樓

		自動(dòng)登錄	找回密碼
密碼			To register

關(guān)于派博傳思			派博傳思旗下網(wǎng)站			友情鏈接
派博傳思介紹	公司地理位置	論文服務(wù)流程	影響因子官網(wǎng)	吾愛(ài)論文網(wǎng)	大講堂	北京大學(xué)	Oxford Uni.	Harvard Uni.
發(fā)展歷史沿革	期刊點(diǎn)評(píng)	投稿經(jīng)驗(yàn)總結(jié)	SCIENCEGARD	IMPACTFACTOR	派博系數(shù)	清華大學(xué)	Yale Uni.	Stanford Uni.
\|Archiver\|手機(jī)版\|小黑屋\| 派博傳思國(guó)際 ( 京公網(wǎng)安備110108008328) GMT+8, 2026-1-25 02:54
Copyright © 2001-2015 派博傳思京公網(wǎng)安備110108008328 版權(quán)所有 All rights reserved