KC-135 POWER SPECTRAL VERTICAL GUST LOAD ANALYSIS. VOLUME 2. SUPPLEMENTARY RESULTS
Abstract
This document presents frequency response functions, power spectra, and response parameters of bending moments, shears, and torsions at two wing stations and two body stations for five conditions of speed, gross weight, and altitude. Volume 1 presents frequency response functions and response parameters for stresses at the same wing and body stations. Also presented in volume 1 are ratios of incremental allowable limit stress to stress response parameter.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1966
- Accession Number
- AD0806913
Entities
People
- Robert N. Latz
Organizations
- Boeing Commercial Airplanes