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Bibliografia 1 Eduard Perez: Ariane 5 User’s Manual, Issue 5 Revision 1 luglio 2011, pubblicato su www.arianespace.com 2 Denis Gély, Georges Elias, Flavia Mascanzoni, Henri Foulon: Acoustic Environment of the VEGA Launch Vehicle at Lift-Off; Atti del ForumAcusticum 2005 (pagg. 821÷826) 3 Max Kandula: Prediction of Turbulent Jet Mixing Noise Reduction by Water Injection; distribuito dalla NASA Center for Aerospace Information (CASI), www.nasa.com 4 Max Kandula: Broadband shock noise reduction in turbulent jet by water injection. Distribuito dalla NASA Center for Aerospace Information (CASI), www.nasa.com; www.nasa.gov 5 Marino Fragnito, Jean-Luc Parquet, Michel Bonnet: Vega Launcher System Test Campaign, From LV Environment to Payload Acoustic Specification, Atti dell’European Conference on Spacecraft Structures, Materials & Mechanical Testing, Nordwijk (Olanda) 10-12 maggio 2005 (ESA SP-581 Agosto 2005) 6 D.G. Crighton: Orderly structure as a source of jet exhaust noise, Survey lecture, In Structure and Mechanism of Turbulence II (editrice Fieldler), Lecture Notes in Physics, volume 76, pagine 154-170, Springer 1977

7 N.S. Dougherty, S.H. Guest: A correlation of scale model and flight aeroacoustic data for the Space Shuttle vehicle, AIAA-84-2351, AIAA/NASA 9th Aeroacoustics Conference, Williamsburg, Virginia, Ottobre 1984 8 J.H. Jones: Scaling of ignition startup pressure transients in rocket systems as applied to the space shuttle overpressure phenomenon, JANNAF 13th Plume Technology Meeting, CPIA-PUB357, Vol. 1, 1982 9 V. Morinie, Y. Gervais, J.L. Peube: Numerical calculation of spectrum emission and jet noise reduction by injection of mass, Internoise 95, Newport Beach, pagine 273-276, Luglio 1995 10 A. Roshko:Experiments on the flow past a circular cylinder at very high Reynolds number, 15 Novembre 1960, pagg. 345-356, Guggenheim Aeronautical Laboratory, California Institute of Technology, Pasadena, California 11 Boye Ahlborna, Mae L. Setob, Bernd R. Noackc: On drag, Strouhal number and vortex-street structure, Fluid Dynamics Research n.30 (anno 2002) pagg. 379–399, Elsevier 12 S.G. Popov: Dependence between the Strouhal and Reynolds numbers in two dimensional flow past a circular cylinder, Nasa Technical Translation, Washington D.C. 20546, 1966, NASA TT F-1 1,763

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