Development of a Full-Range Transducer Assembly for the Generation of High Intensity Sound

Liebich RE, King JA. Development of a Full-Range Transducer Assembly for the Generation of High Intensity Sound. In: AES Convention 10. Audio Engineering Society; 1958.pp. 71:1-13. Available from: https://aes.org/publications/elibrary-page/?id=151

@inproceedings{Liebich1958_151,
  author = {Liebich, Richard E. and King, John A.},
  title = {{Development of a Full-Range Transducer Assembly for the Generation of High Intensity Sound}},
  booktitle = {AES Convention 10},
  pages = {71:1-13},
  url = {https://aes.org/publications/elibrary-page/?id=151},
  year = {1958},
  month = sep,
  publisher = {Audio Engineering Society}
}

TY  - CPAPER
TI  - Development of a Full-Range Transducer Assembly for the Generation of High Intensity Sound
AU  - Liebich, Richard E.
AU  - King, John A.
T2  - AES Convention 10
SP  - 1
EP  - 13
M1  - Paper 71
PY  - 1958
DA  - 1958/09/06
UR  - https://aes.org/publications/elibrary-page/?id=151
PB  - Audio Engineering Society
LA  - en
AB  - The requirements of the aircraft industry for environmental testing of electronic components in high intensity sound fields have led to the development of a high-energy, full-frequency-range coaxial transducer assembly. The high acoustic output range from 16 to 18,000 cycles is generated by a low frequency cone employing a unique suspension system, a mid-frequency horn-loaded compression driver, and a group of inductively driven high frequency radiators, all mounted symmetrically within a cast metal frame eighteen inches square.
ER  -