Vertical Wind Tunnel for Prediction of Rocket Flight Dynamics-Reference-Cited by-同舟云学术

Vertical Wind Tunnel for Prediction of Rocket Flight Dynamics

Published:2016-03-29 Issue:2 Volume:3 Page:10
ISSN:2226-4310
Container-title:Aerospace
language:en
Short-container-title:Aerospace

Author:

Bryson Hoani,Sültrop Hans,Buchanan George,Hann Christopher,Snowdon Malcolm,Rao Avinash,Slee Adam,Fanning Kieran,Wright David,McVicar Jason,Clark Brett,Harris Graeme,Chen Xiao

Publisher

MDPI AG

Subject

Aerospace Engineering

Link

http://www.mdpi.com/2226-4310/3/2/10/pdf

Reference19 articles.

1. UC Rocketry Projecthttp://ucrocketry.org/

2. Description and Flow Assessment of the Delft Hypersonic Ludwieg Tube

3. Numerical Investigation of Canard-Controlled Missile with Planar and Grid Fins

4. Effect of Canard Interactions on Aerodynamic Performance of a Fin-Stabilized Projectile

Cited by 5 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. New Zealand’s Growing Space Sector: A Technological and Science Perspective;Space Law and Policy;2024

2. Design and Implementation of Flight Computer for Sounding Rockets - S3FC;2022 6th International Conference on Electronics, Communication and Aerospace Technology;2022-12-01

3. Utilization of Wind Tunnels for Subsonic and Transonic Flow for Aeronautical and Non-aeronautical Applications: A Review;Journal of The Institution of Engineers (India): Series C;2021-09-22

4. The Two-Point Boundary-Value Problem for Rocket Trajectories;Aerospace;2020-09-02

5. Wind Tunnel Tests of Influence of Boosters and Fins on Aerodynamic Characteristics of the Experimental Rocket Platform;Transactions on Aerospace Research;2017-12-01