Accession Number : AD0428181


Title :   A RATIONAL METHOD FOR PREDICTING ALIGHTING GEAR DYNAMIC LOADS. VOLUME II EXAMPLES.


Descriptive Note : Rept. for 2 Feb 61-30 June 62,


Corporate Author : CHANCE VOUGHT CORP DALLAS TEX


Personal Author(s) : Ferguson,T R ; Mollick,J ; Kitts,W W


Report Date : Dec 1963


Pagination or Media Count : 273


Abstract : Several illustrative examples, with accompanying numerical solutions are provided as a didactic means of illustrating how the ''General Method'', Volume I (AD-428 027), is applied to various landing impact problems. Symmetrical landing of a conventional aircraft, asymmetrical landing of an advanced vehicle, spike penetration landing, cantilevered, articulated and semi-articulated gears are considered. (Author)


Descriptors :   *LANDING GEAR , LOADS(FORCES) , MOTION , AIRFRAMES , AIRCRAFT PANELS , LANDING IMPACT , IMPACT , GRAVITY , AIRCRAFT TIRES , SPIKES , PENETRATION , HYDRAULIC EQUIPMENT , HYDRAULIC CYLINDERS , ELASTIC PROPERTIES , DEFLECTION , MATHEMATICS


Distribution Statement : APPROVED FOR PUBLIC RELEASE