GaltonF. (1883) Hydrogen whistles. Nature, Vol. 27, pp. 491–492.
2.
ChanaudR.C. (1963) Experiments concerning the vortex whistle. J. Acoust. Soc. Am., Vol. 35, pp. 953–960.
3.
VonnegutB. (1954) A vortex whistle. J. Acous. Soc. Am., Vol. 26, No. 1, pp. 18–20.
4.
PowellA. (1953) On the noise emanating from a two-dimensional jet above the critical pressure. Aeronautical Quarterly, Vol. 4, pp. 103–122.
5.
RamanG. (1998) Advances in understanding supersonic jet screech: Review and perspective. Prog. Aero. Sci., Vol. 34, pp.45–106.
6.
RamanG. (1999) Supersonic jet screech: Half-century from Powell to the present. J. Sound & Vib., 225, No. 3, pp. 543–571.
7.
HartmannJ. (1919) Om en ny methode til frembringelse af lydsvinginger. Dan. Mat. Fys. Medd., Vol. 1, p. 13.
8.
HartmannJ. (1922) On a new method for the generation of sound waves. Phys. Rev., Vol. 20, pp. 719–727.
9.
SprengerH. (1954) Über thermische Effekte bei Reseonanzrohren, Mitt. Inst. Aerodynamik, ETH, vol. 21, pp. 18–35.
10.
HartmannJ. (1936) The Hartmann acoustic generators. Engineering, Vol. 142, pp. 491–492.
11.
HartmannJ. (1939) Construction, Performance and Design of the Acoustic Air-Jet Generator, J. Sci. Instr., Vol. 16, pp. 140–149.
12.
HartmannJ.LazarusF. (1940) The radiation of the acoustic air-jet generator derived from direct observations of the amplitude of the aerial vibrations of the oscillator. Phil. Mag., Vol. 29, pp. 140–147.
13.
SmithT.J.B.PowellA. (1964) Experiments concerning the Hartmann Whistle, Report 64–42, Department of Engineering, UCLA.
14.
SavoryE. (1950) Experiments with the Hartmann Acoustic Generator, Engineering, Vol. 170, pp. 99–100.
15.
HartmannJ.TrusdøE. (1951) Synchronisation of air-jet generators with an appendix on the stem generator. Dan. Mat. Fys. Medd., Vol. 26, p. 10.
16.
RamanG.KibensV. (2001) Active flow control using integrated powered resonance tube actuators. AIAA Paper 2001–3024.
17.
AckeretJ. (1961) The Role of entropy in the aerospace sciences- Daniel and Florence Guggenheim Memorial Lecture. J. Aero. Sci., Vol. 28, No.2, pp. 81–95.
18.
IwamotoJ. (1986) Necessary conditions for starting and maintaining a stable oscillatory flow in a Hartmann-Sprenger tube”, Flow Visualization, IV, 507.
19.
GregussP. (1964) The application of airborne and liquid-borne sounds to industrial technology. Ultrasonics, Vol. 2, pp. 5–10.
20.
KibensV.RamanG. (2002) High frequency excitation apparatus and method for reducing jet and cavity noise. US Patent No. 6,375,118, April 23, 2002.
21.
RamanG.KhanafsehS.CainA.B.KerschenE.J. (2004) Development of high bandwidth powered resonance tube actuators with feedback control. J. Sound & Vib., Vol. 269, pp. 1031–1062.
