Need for full scale inflight verification of subcritical aeroelastic characteristics of advanced aircraft; flight flutter techniques, development of impulsive excitation techniques and suitable ballistic devices as means of exciting structure; response measuring system and data analysis; theoretical subcritical response; comparison of experimental and theoretical results; FJ-4 aircraft development program, and A3J-1 flight program; recommendations.
Application of impulsive excitation to in-flight vibration testing
Aerospace Eng
Aerospace Engineering ; 20 , n 1
1961
Article (Journal)
English
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