Page 47 - Winter2018
P. 47
References
Allgood, D. C., Saunders, G. P., and Langford, L. A. (2014). Reduction of altitude diffuser jet noise using water injection. In Proceedings of the 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, TN, January 9-12, 2012.
Arenas, J. P., and Margasahayam, R. (2006). Noise and vibration of space- craft structures. Ingenaire: Revista Chilena de Ingenieria 14, 251-328.
Bies, D. A., and Franken, P. A. (1961). Notes on scaling jet and rocket noise. The Journal of the Acoustical Society of America 33, 1171-1173.
Caimi, R. E., and Margasahayam, R. (1997). Validation of a Deterministic Vibroacoustic Response Prediction Model. National Aeronautics and Space Administration (NASA) Technical Memorandum 112649, NASA, Wash- ington, DC. Available at https://go.nasa.gov/2og40ig.
Casalino, D., Santini, S., Genito, M., and Ferrara, V. (2012). Rocket noise sources localization through a tailored beamforming technique. American Institute of Aeronautics and Astronautics Journal 50, 2146-2158.
Eldred, K. M., and Jones, G. W., Jr. (1971). Acoustic Loads Gener- ated by the Propulsion System. National Aeronautics and Space Ad- ministration (NASA) SP 8072, NASA, Washington, DC. Available at https://go.nasa.gov/2BPZVeE.
Fukuda, K., Fujii, K., Ui, K., Ishii, T., Oinuma, H., Kazawa, J., and Minesugi, K. (2009). Acoustic measurements and prediction of solid rockets in static firing tests. In Proceedings of the 15th AIAA/CEAS Aeroacoustics Confer- ence (30th AIAA Aeroacoustics Conference), Miami, FL, May 11-13, 2009, p. 3368.
Gee, K. L., Giraud, J. H., Blotter J. D., and Sommerfeldt, S. D. (2010). Near- field vector intensity measurement of a small solid rocket motor. The Jour- nal of the Acoustical Society of America 128, EL69-EL74.
Gee, K. L., Neilson, T. B., and James, M. (2014). Including source correla- tion and atmospheric turbulence in a ground reflection model for rock- et noise. Proceedings of Meetings on Acoustics 22, 040001. Available at https://doi.org/10.1121/2.0000002.
Gely, D., Elias, G., Bresson, C., Foulon, H., and Radulovic, S. (2000). Reduc- tion of supersonic jet noise. Application to the Ariane V launch vehicle. In Proceedings of the 6th Aeroacoustics Conference and Exhibit, Lahaina, HI, June 12-14, 2000, p. 2026.
Gely, D., Elias, G., Mascanzoni, F., and Foulon, H. (2005). Acoustic environ- ment of the VEGA launch vehicle at lift-off. In Proceedings of the Forum Acusticum, Budapest, Hungary, August 29 to September 2, 2005, pp. 821- 826.
Giacomoni, C., and Kenny, R. J. (2016). Comparison of spatial corre- lation parameters between full and model scale launch vehicles. The Journal of the Acoustical Society of America 140, 3043. Available at https://go.nasa.gov/2oHKHyP.
Giraud, J. H., Gee, K. L., and Ellsworth, J. E. (2010). Acoustic temperature measurement in a rocket noise field. The Journal of the Acoustical Society of America 127, EL179-EL184.
Goddard, R. H. (2002). Rockets: Two Classic Papers, Dover, New York. Guest, S., and Jones, J. H. (1967). Far-Field Acoustics Environmental Predic- tions for Launch of Saturn V and Saturn V MLV Configuration. National Aeronautics and Space Administration (NASA) Technical Note D-4117,
NASA, Washington, DC. Available at https://go.nasa.gov/2odMg7. Herting, D. N., Joseph, J. A., Kuusinen, L. R., and MacNeal, R. H. (1971). Acoustic Analysis of Solid Motor Rocket Cavities by a Finite Element Meth- od. National Aeronautics and Space Administration (NASA) Technical
Memorandum X-2378, NASA, Washington, DC.
Hess, R. W., Fralich, R. W., and Hubbard, H. H. (1957). Studies of Structural
Failure Due to Acoustic Loading. National Advisory Committee for Aero- nautics (NACA) Technical Note 4050, NACA, Washington, DC. Available at https://go.nasa.gov/2BOeuix.
Houston, J., Counter, D., and Giacomoni, C. (2015). SLS scale model acous- tic test liftoff results and comparisons. In Proceedings of the 29th Aerospace Testing Seminar, Los Angeles, CA, October 27-29, 2015.
Humphrey, A. J. (1957). Rocket noise environments. The Shock and Vibra- tion Bulletin No. 25, Pt. II, pp. 10-17.
Klotz, I. (2017). Recycling rockets. Aerospace America 55(8), 32-37. Koudriavtsev, V., Varnier, J., and Safronov, A. (2004). A simplified model of jet aerodynamics and acoustics. In Proceedings of the 10th AIAA/CEAS
Aeroacoustics Conference, Manchester, UK, May 10-12, 2004, p. 2877. Krothapalli, A., Venkatakrishnan, L., Lourenco, L., Greska, B., and Ela- varasan, R., (2003). Turbulence and noise suppression of a high-speed jet
by water injection. Journal of Fluid Mechanics 491, 131-159.
Lambare, H. (2016). Acoustical design of the ELA4 launch pad for the Ari- ane 6 launcher. The Journal of the Acoustical Society of America, 140, 3422.
Available at https://bit.ly/2NqpPKB.
Lighthill, M. J. (1952). On sound generated aerodynamically. I. General
theory. Proceedings of the Royal Society of London A: Mathematics, Physi-
cal and Engineering Sciences 211, 564-587.
Lighthill, M. J. (1954). On sound generated aerodynamically. II. Turbulence
as a source of sound, Proceedings of the Royal Society of London A: Math-
ematics, Physical and Engineering Sciences. 222(1148), 1-32.
Lubert, C. P. (2008). Application of turbulent mixing noise theory to flows over Coanda surfaces. International Journal of Acoustics and Vibration 13,
17-30.
Lubert, C. P. (2017). Sixty years of launch vehicle acoustics. Proceedings of
Meetings on Acoustics, 31, 040004. Available at https://bit.ly/2LVoUgh. Margasahayam, R., Caimi, R. E., and Hauss, S. (2002). Rocket launch trajec- tory simulation mechanism. In Proceedings of the 9th International Con-
gress on Sound and Vibration, Orlando, FL, July 8-11, 2002.
Martinez-Val, R., and Perez, E. (2009). Aeronautics and astronautics: Re- cent progress and future trends. Proceedings of the Institution of Mechani- cal Engineers Part C: Journal of Mechanical Engineering Science 223, 2767-
2820.
Merriam-Webster Dictionary New Edition. (2016). The Merriam-Webster
Dictionary New Edition. Merriam-Webster, Inc., Springfield, MA. Morgan, J., Neilsen, T. B., Gee, K. L., Wall, A. T., and James, M. M. (2012). Simple-source model of military jet aircraft noise. Noise Control Engineer-
ing Journal 60(4), 435-449.
Natarajan, K., and Venkatakrishnan, L. (2016). Influence of launch platform
cut-outs on flow and acoustic behavior of rocket exhaust. The Journal of
the Acoustical Society of America 140, 3042.
Norum, T. D. (2004). Reductions in multi-component jet noise by water
injection. In Proceedings of the 10th AIAA/CEAS Aeroacoustics Conference,
Manchester, UK, May 10-12, 2004.
Panda, J., Mosher, R. N., and Porter, B. J. (2013). Identification of Noise
Sources During Rocket Engine Test Firings and a Rocket Launch Using a Mi- crophone Phased-Array. National Aeronautics and Space Administration (NASA) Technical Memorandum 2013-216625, NASA, Washington, DC. Available at https://go.nasa.gov/2oaChQj.
Pico, R., Herrero-Dura, I., Sanchez-Morcilli, V., Salmeron-Contreras, L. J., and Garcia-Raffi, L. M. (2016). Acoustic behaviour of the VEGA launch pad environment. EuroRegio 2016 Conference, Porto, Portugal, June 13-15, 2016.
Plotkin, K., Sutherland, L., and Vu, B. (2009). Liftoff acoustics predictions for the Ares I launch pad. In Proceedings of the 15th AIAA/CEAS Aero- acoustics Conference (30th AIAA Aeroacoustics Conference), Miami, FL, May 11-13, 2009, p. 3163.
Teitel, A. S. (2016). How the noise of big rockets breaks apart buildings. Popular Science, October 10, 2016.
Tsiolkovsky, K. E. (1903). The exploration of cosmic space by means of reac- tion devices. Scientific Review 5.
Winter 2018 | Acoustics Today | 45