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.
Authors:
Liebich, Richard E.; King, John A.
Affiliation:
Stromberg-Carlson, A Division of General Dynamics Corporation, Rochester, NY
AES Convention:
10 (September 1958)
Paper Number:
71
Publication Date:
September 1, 1958
Click to purchase paper as a non-member or you can login as an AES member to see more options.
No AES members have commented on this paper yet.
To be notified of new comments on this paper you can subscribe to this RSS feed. Forum users should login to see additional options.
If you are not yet an AES member and have something important to say about this paper then we urge you to join the AES today and make your voice heard. You can join online today by clicking here.