Rice EJ. Attenuation of sound in ducts with acoustic treatment – a generalized approximate equation. NASA TM X-71830, presented at the 90th Meeting of the Acoustical Society of America, November 1975.
2.
RiceEJ. Inlet noise suppressor design method based upon the distribution of acoustic power with mode cut-off ratio. Adv Engi Sci1976; III: 883[NASA CP-2001].
3.
Rice EJ.Modal density function and number of propagating modes in ducts. NASA TM X-73539. In: The 92nd meeting of the acoustical society of America, San Diego, CA, November 16–19, 1976.
Rice EJ. Aircraft inlet noise radiation model; static, flight and bellmouth effect. AIAA 96-1774. In: The 2nd AIAA/CEAS aeroacoustics conference, State College, PA, 6–8 May, 1996.
6.
Rice EJ. Broadband noise radiation models for aircraft engines. AIAA 99-1953. In: The 5th AIAA/CEAS aeroacoustics conference, Greater Seattle, Washington, 10–12 May, 1999.
7.
Rice EJ. A theoretical study of the acoustic impedance of orifices in the presence of a steady grazing flow. NASA TM X-71903. In: 91st Meeting of the Acoustical Society of America, Washington DC, April 5–9, 1976.
8.
Baumeister KJ and Rice EJ. Visual study of the effect of grazing flow on the oscillatory flow in a resonator orifice. NASA TM X-3288, September 1975.
9.
Rice EJ. A model for the acoustic impedance of linear suppressor materials bonded on perforated plate. AlAA Paper 81-1999. In: The 7th AlAA aeroacoustics conference, Palo, CA, 5–7 October, 1981. (also NASA TM 82716).
10.
Heidelberg LJ, Rice EJ and Homyak L. Experimental evaluation of a spinning-mode acoustic treatment design concept for aircraft inlets. NASA TP-1613, April, 1980.
11.
RiceEJHeidelbergLJ. Comparison of inlet suppressor data with approximate theory based on cutoff ratio. J Aircraft1981; 18: 810.
