A RATIONAL METHOD FOR PREDICTING ALIGHTING GEAR DYNAMIC LOADS. VOLUME II EXAMPLES.
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1963
- Accession Number
- AD0428181
Entities
People
- J. Mollick
- T. R. Ferguson
- W. W. Kitts
Organizations
- Vought