Accession Number : AD0735472

Title :   Statistical Methods and Their Application to Establishing Flight Maneuver Loads Design Criteria for Fighter Aircraft.

Descriptive Note : Summary rept.,

Corporate Author : NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AERO STRUCTURES DEPT

Personal Author(s) : De Fiore,Thomas A. ; Stewart,William C.

Report Date : 01 SEP 1971

Pagination or Media Count : 54

Abstract : The report provides statistical methods for use in establishing positive maneuver loads design criteria for fighter aircraft. These methods are applied to counting accelerometer data and comparisons between operational loads data and military specifications are presented. (Author)

Descriptors :   (*NAVAL AIRCRAFT, *AERODYNAMIC LOADING), JET FIGHTERS, GRAVITY, CORRELATION TECHNIQUES, MULTIVARIATE ANALYSIS, CLIMBING, ACCELERATION, ACCELEROMETERS

Subject Categories : Attack and Fighter Aircraft
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE