Accession Number : ADA952090

Title :   Stability Derivatives for Delta Wings and Slender Bodies by the Linearized Theory,

Corporate Author : PRINCETON UNIV NJ JAMES FORRESTAL RESEARCH CENTER

Personal Author(s) : Wald, Quentin

Report Date : 01 JUL 1947

Pagination or Media Count : 32

Descriptors :   *DELTA WINGS, *AERODYNAMIC STABILITY, WING BODY CONFIGURATIONS, SLENDER BODIES, EQUATIONS OF MOTION, DERIVATIVES(MATHEMATICS), LINEAR SYSTEMS, THEORY, YAW, PITCH(MOTION), BODIES OF REVOLUTION.

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE