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