Accession Number : AD0112452


Title :   LONGITUDINAL AIRPLANE DYNAMICS WIND TUNNEL TEST EQUIPMENT


Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO NY


Personal Author(s) : TUFTS, O.B. ; DURYEA, G.R. JR.


Report Date : JUL 1955


Pagination or Media Count : 1


Descriptors :   *WIND TUNNEL MODELS), (*JET FIGHTERS, (*AIRPLANE MODELS), AERODYNAMIC CHARACTERISTICS, PITCH(MOTION), VIBRATION, FREQUENCY, MACH NUMBER, TURBULENCE, INSTRUMENTATION, SUBSONIC CHARACTERISTICS, AERODYNAMIC LOADING, LOADS(FORCES).


Distribution Statement : APPROVED FOR PUBLIC RELEASE