Accession Number : ADA951971

Title :   Methods for Obtaining Aerodynamic Data through Steady State Flight Testing. Part 2. The Lateral Derivatives,

Corporate Author : PRINCETON UNIV N J JAMES FORRESTAL RESEARCH CENTER

Personal Author(s) : Perkins,Courtland D.

Report Date : 03 DEC 1950

Pagination or Media Count : 47

Descriptors :   *Aerodynamic stability, *Turning flight, Data acquisition, Derivatives(Mathematics), Flight testing, Steady state, Ailerons, Aerial rudders, Trim(Aerodynamics), Sideslip, Skidding, Roll, Equations of motion

Subject Categories : Test Facilities, Equipment and Methods

Distribution Statement : APPROVED FOR PUBLIC RELEASE