Accession Number : AD0287668

Title :   METHODS OF SELECTION AND APPROXIMATE CALCULATION OF AIR DESIGN PARAMETERS

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date : 27 SEP 1962

Pagination or Media Count : 1

Abstract : Specific problems in aicraft design are studied. They include airspeed determination of supesonic aircraft; seleion of optimum number of turbojet engines; determination of fuselage slendernessratio; wing weight determination; determination of the parameters of brake assembly design; aircraft trim deterinations for aircraft wth tricycle landing gear; determination of the type and calculation of the rigidity of the trutural stiffening system. (Author)

Descriptors :   *AIRFRAMES, *JET AIRCRAFT, AERODYNAMIC CHARACTERISTICS, AIRCRAFT, CIVIL AVIATION, EQUATIONS, FRICTION, FUSELAGES, LANDING GEAR, LOAD DISTRIBUTION, MATHEMATICAL ANALYSIS, PARACHUTES, SHEAR STRESSES, STIFFENED CYLINDERS, SUPERSONIC AIRCRAFT, THEORY, TRIM TABS, TURBOJET ENGINES, VELOCITY, WINGS

Distribution Statement : APPROVED FOR PUBLIC RELEASE