Z(XQ-5)ZTEST WING VIBRATION TEST.
Abstract
An XQ-5 test wing mounted in a supporting fixture, was subjected to vibratory excitations of 10 to 150 cps to determine resonant frequencies, relative amplitudes, node line locations and damping coefficients. The test yielded reasonably satisfactory data which enabled accomplishment of its purpose. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 11, 1956
- Accession Number
- AD0370569
Entities
People
- A. T. Lien
Organizations
- Lockheed Martin