Skip to Main Content
Close
Journals
Books
Case Studies
Collections
Open Access
Citation Manager
Journals
Books
Case Studies
Collections
Open Access
Citation Manager
Search Dropdown Menu
header search
search input
Search input auto suggest
filter your search
All Content
All Journals
Aircraft Engineering and Aerospace Technology: An International Journal
Search
Advanced Search
Cart
User Tools Dropdown
Cart
Register
Sign In
Open Menu
Aircraft Engineering and Aerospace Technology: An International Journal
Toggle Menu
Menu
Journal Home
Issues
About this Journal
Open External Link
Earlycite Articles
Issues
Select Decade
2020
2010
2000
1990
1980
1970
1960
1950
1940
1930
1920
Select Year
2019
2018
2017
2016
2015
2014
2013
2012
2011
2010
Issue
18 January - Volume 85, Issue 1, Pages 4 - 81
15 March - Volume 85, Issue 2, Pages 87 - 160
3 May - Volume 85, Issue 3, Pages 171 - 244
28 June - Volume 85, Issue 4, Pages 247 - 339
30 August - Volume 85, Issue 5, Pages 343 - 431
14 October - Volume 85, Issue 6, Pages 435 - 496
20 December - Volume 86, Issue 1, Pages 6 - 86
Volume 85, Issue 4
28 June 2013
Editors
Phil Webb
Phil Webb
Search for other works by this author on:
This Site
PubMed
Google Scholar
All Issues
Cover Image
Cover Image
ISSN
1748-8842
EISSN
1758-4213
Close navigation menu
Issue Navigation
Numerical study on effect of leading‐edge tubercles
Zhang Xingwei
;
Zhou Chaoying
;
Zhang Tao
;
Ji Wenying
Abstract
View article
titled, SCM.SharedControls.Infrastructure.TitleDisplayModel?.Text
Open the
PDF
for in another window
Add to Citation Manager
for Numerical study on effect of leading‐edge tubercles
Double‐layer fusion algorithm for EGI‐based system
Rong Wang
;
Jianye Liu
;
Zhi Xiong
;
Qinghua Zeng
Abstract
View article
titled, SCM.SharedControls.Infrastructure.TitleDisplayModel?.Text
Open the
PDF
for in another window
Add to Citation Manager
for Double‐layer fusion algorithm for EGI‐based system
Aerodynamic parameter estimation using adaptive unscented Kalman filter
M. Majeed
;
Indra Narayan Kar
Abstract
View article
titled, SCM.SharedControls.Infrastructure.TitleDisplayModel?.Text
Open the
PDF
for in another window
Add to Citation Manager
for Aerodynamic parameter estimation using adaptive unscented Kalman filter
Effects of characteristic geometric parameters on parafoil lift and drag
Yihua Cao
;
Xu Zhu
Abstract
View article
titled, SCM.SharedControls.Infrastructure.TitleDisplayModel?.Text
Open the
PDF
for in another window
Add to Citation Manager
for Effects of characteristic geometric parameters on parafoil lift and drag
Parameters determination for concept design of solar‐powered, high‐altitude long‐endurance UAV
Gao Xian‐Zhong
;
Hou Zhong‐Xi
;
Guo Zheng
;
Zhu Xiong‐Feng
;
Liu Jian‐Xia
;
Chen Xiao‐Qian
Abstract
View article
titled, SCM.SharedControls.Infrastructure.TitleDisplayModel?.Text
Open the
PDF
for in another window
Add to Citation Manager
for Parameters determination for concept design of solar‐powered, high‐altitude long‐endurance UAV
Contra‐rotating propeller for fixed wing MAV: part 1
Jacek Mieloszyk
;
Cezary Galiński
;
Janusz Piechna
Abstract
View article
titled, SCM.SharedControls.Infrastructure.TitleDisplayModel?.Text
Open the
PDF
for in another window
Add to Citation Manager
for Contra‐rotating propeller for fixed wing MAV: part 1
Contra‐rotating propeller for fixed wing MAV: part 2
Jacek Mieloszyk
;
Cezary Galiński
;
Janusz Piechna
;
Jacek Brzozowski
Abstract
View article
titled, SCM.SharedControls.Infrastructure.TitleDisplayModel?.Text
Open the
PDF
for in another window
Add to Citation Manager
for Contra‐rotating propeller for fixed wing MAV: part 2
Instrumented flight test of flapping micro air vehicle
Jong Heon Kim
;
Chan Yik Park
;
Seung Moon Jun
;
Gregory Parker
;
Kwang Joon Yoon
;
Dae Keun Chung
;
Il Hyun Paik
;
Jong Rok Kim
Abstract
View article
titled, SCM.SharedControls.Infrastructure.TitleDisplayModel?.Text
Open the
PDF
for in another window
Add to Citation Manager
for Instrumented flight test of flapping micro air vehicle
Latest
Most Read
Most Cited
Robust longitudinal control for a hypersonic glider with moving-mass actuation via L1-augmented dynamic inversion
Nonlinear geometric multivariable control for unmanned aircraft flight system
Numerical simulation of strut angle optimization for enhanced performance in DLR scramjet combustor
Active disturbance rejection control optimized via chaotic comprehensive learning pigeon-inspired optimization for flapping-wing aerial vehicle
Email alerts
Earlycite Alert
Closed Issue Alert
Latest Published Articles Alert
Close Modal
Recommended for you
These recommendations are informed by your reading behaviors and indicated interests.
RSS
Current Issue RSS Feed
RSS Feed - Advance Access
Open Issues RSS Feed
Close Modal
Close Modal
This Feature Is Available To Subscribers Only
Sign In
or
Create an Account
Close Modal
Close Modal