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Method for Determining the Frequency-response Characteristics of an Element of System from the System Transient Output Response to a Known Input Function
United States. National Advisory Committee for Aeronautics
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United States. National Advisory Committee for Aeronautics
Method for Determining the Frequency-response Characteristics of an Element of System from the System Transient Output Response to a Known Input Function
United States. National Advisory Committee for Aeronautics,
Charles W. Matthews,
Clinton E. Brown,
E. B. Klunker,
Harold Mirels,
Howard J. Curfman,
John A. Zalovcik,
John C. Sanders,
Edward C. Chapin,
H. Reese Ivey,
Robert A. Gardiner,
Rogers Thompson,
Rudolph C. Haefeli
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