Accession Number:

AD0806913

Title:

KC-135 POWER SPECTRAL VERTICAL GUST LOAD ANALYSIS. VOLUME 2. SUPPLEMENTARY RESULTS

Descriptive Note:

Final technical rept. 1 Jul 1965-1 Jun 1966

Corporate Author:

BOEING COMMERCIAL AIRPLANE CO RENTON WA

Personal Author(s):

• Latz, Robert N.

Report Date:

1966-07-01

Pagination or Media Count:

256.0

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.

Descriptors:

• *ATMOSPHERIC MOTION
• *JET TRANSPORT AIRCRAFT
• ALTITUDE
• BENDING
• FLIGHT SPEEDS
• FUSELAGES
• GUST LOADS
• MEASUREMENT
• NACELLES
• POWER SPECTRA
• SWEPTBACK WINGS
• TANKER AIRCRAFT
• WEIGHT
• WIND

Subject Categories:

• Transport Aircraft
• Atmospheric Physics
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE