Accession Number : AD0110443


Title :   THE DETERMINATION OF HELICOPTER LOGITUDINAL STABILITY DERIVATIVES FROM FLIGHT TEST DATA. PART I. DEVELOPMENT OF FLIGHT TEST INSTRUMENTATION. TECHNIQUES AND ANALYSIS METHODS


Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO NY


Personal Author(s) : DEAZLEY, W R ; SCHULTZ, E R


Report Date : Feb 1958


Pagination or Media Count : 140


Descriptors :   *FLIGHT TESTING , *STABILITY , *HELICOPTERS , MATHEMATICAL ANALYSIS , INSTRUMENTATION


Distribution Statement : APPROVED FOR PUBLIC RELEASE