Accession Number : ADA956532

Title :   Trim Requirements and Static-Stability Derivatives from a Wind-Tunnel Investigation of a Lifting Rotor in Transition.

Descriptive Note : Technical note,

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HAMPTON VA LANGLEY RESEARCH CEN TER

Personal Author(s) : Jenkins, Julian L., Jr

Report Date : FEB 1965

Pagination or Media Count : 40

Descriptors :   *AERODYNAMIC STABILITY, *WIND TUNNEL TESTS, LIFT, ROTARY WING AIRCRAFT.

Subject Categories : Aerodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE