Pressure Fluctuations in the Transonic Boundary Layer of a VEGA Launcher Model-Reference-Cited by-同舟云学术

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Pressure Fluctuations in the Transonic Boundary Layer of a VEGA Launcher Model

Published:2005-05-23 Issue: Volume: Page:
ISSN:
Container-title:11th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Guj Giulio¹,Camussi Roberto¹,Di Marco Alessandro¹,Imperatore Biagio²

Affiliation:

1. University 'Roma 3'

2. CIRA - Italian Aerospace Research Centre

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2856

Reference15 articles.

1. VEGA, a small launch vehicle

2. 2Imperatore,B.,Guj,G.,Ragni,A.,Pizzicaroli,A.andGiulietti,E."AeroacousticoftheVEGALauncher:Wind TunnelTests andFullScale Extrapolations",AIAApaper2005-2913,2005.

3. Experimental investigation of the base flow and base pressure of a clustered launch vehicle

4. A COMPARISON OF MODELS FOR THE WAVENUMBER–FREQUENCY SPECTRUM OF TURBULENT BOUNDARY LAYER PRESSURES

Cited by 1 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. Aeroacoustics research in Europe: The CEAS-ASC Report on 2005 highlights;Journal of Sound and Vibration;2007-01

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