BLAST RESPONSE OF A TYPICAL AIRCRAFT FUSELAGE STRUCTURE Open PDF Document Details Document Type Technical Report Publication Date Mar 20, 1962 Accession Number AD0275080 Entities People N. L. Basdekas R. C. Dehart Organizations Southwest Research Institute Tags Communities of Interest Air Platforms DTIC Thesaurus Topics Bending Moments Bending Stress Complex Variables Coordinate Systems Difference Equations Differential Equations Dynamic Loads Dynamic Pressure Dynamic Response Equations Frequency Fuselages Government Procurement Modulus Of Elasticity Numerical Integration Resonant Frequency Vibration