Development of a Low Cost Dynamic Wind Tunnel Facility Utilizing MEMS Inertial Sensors-Reference-Cited by-同舟云学术

Development of a Low Cost Dynamic Wind Tunnel Facility Utilizing MEMS Inertial Sensors

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Carnduff Stephen¹,Erbsloeh Sascha¹,Cooke Alastair¹,Cook Mike¹

Affiliation:

1. Cranfield University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-196

Reference24 articles.

1. Wind-Tunnel Technique for Determining Stability Derivatives from Cable-Mounted Models

2. Test installations to investigate the dynamic behaviour of aircraft with scaled models in wind tunnels

3. The wind tunnel behaviour of a scaled model with a gust alleviation system in a deterministic gust field

4. 5Malik, I. A. "The design, development and evaluation of an active control aircraft model wind tunnel facility", Ph.D. thesis,College of Aeronautics, Cranfield Instituteof Technology,1982.

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Identification of aircraft longitudinal aerodynamic parameters using an online corrective test for wind tunnel virtual flight;Chinese Journal of Aeronautics;2024-05

2. Research on Dynamic Characteristics Analysis and Control Law Design Method of Model Aircraft in Wind Tunnel–Based Virtual Flight Testing;Journal of Aerospace Engineering;2023-05

3. Identification of Lateral-Directional Aerodynamic Parameters for Aircraft Based on a Wind Tunnel Virtual Flight Test;Aerospace;2023-04-03

4. Installation error calibration for MEMS angular measurement system in hypersonic wind tunnel;Chinese Journal of Aeronautics;2022-12

5. Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig;Journal of Aircraft;2019-05