Aeroacoustic of the VEGA Launcher: Wind Tunnel Tests and Full Scale Extrapolations

Author:

Imperatore Biagio1,Guj Giulio2,Ragni Antonio1,Pizzicaroli Antonio3,Giulietti Emanuele2

Affiliation:

1. Centro Italiano Ricerche Aerospaziali

2. University 'Roma 3'

3. AVIO S.p.A

Publisher

American Institute of Aeronautics and Astronautics

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. Flow analysis of hammerhead launcher geometries in the transonic regime;AIAA SCITECH 2024 Forum;2024-01-04

2. Experimental study of the boosters impact on the rocket aerodynamic characteristics;Aircraft Engineering and Aerospace Technology;2022-07-21

3. Effect of a Protuberance on Transonic Flowfield around a Rocket Fairing;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2013

4. Aeroacoustics research in Europe: The CEAS-ASC Report on 2005 highlights;Journal of Sound and Vibration;2007-01

5. Pressure Fluctuations in the Transonic Boundary Layer of a VEGA Launcher Model;11th AIAA/CEAS Aeroacoustics Conference;2005-05-23

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