NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Advanced Approaches to Fatigue EvaluationConference on fatigue test evaluation for aircraft structures
Document ID
19720022245
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Structural Mechanics
Report/Patent Number
NASA-SP-309
Meeting Information
Meeting: ICAF Symp.
Location: Miami
Start Date: May 13, 1971
End Date: May 14, 1971
Accession Number
72N29895
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19720022257WorkOn the cyclic stress-strain behavior and low cycle fatigue of aerospace materials19720022263WorkDetection of structural deterioration and associated airline maintenance problems19720022251WorkA proposed USAF fatigue evaluation program based upon recent systems experience19720022258WorkA parametric approach to irregular fatigue prediction19720022248WorkThe Boeing 747 fatigue integrity program19720022256WorkPractical aspects of designing for and evaluating structural integrity19720022265WorkFatigue tests on big structure assemblies of concorde aircraft19720022264WorkFatigue failure of metal components as a factor in civil aircraft accidents19720022246WorkThe Philosophy which underlies the structural tests of a supersonic transport aircraft with particular attention to the thermal cycle19720022253WorkReliability analysis applied to structural tests19720022266WorkStructural testing of concorde aircraft: Further report on United Kingdom tests19720022267WorkA comparison of reliability and conventional estimation of safe fatigue life and safe inspection intervals19720022255WorkFatigue design procedure for the American SST prototype19720022252WorkFatigue Tests with Random Flight Simulation Loading19720022261WorkStatistical analysis of mission profile parameters of civil transport airplanes19720022250WorkThe practical implementation of fatigue requirements to military aircraft and helicopters in the United Kingdom19720022262WorkStatistical load data processing19720022247WorkFatigue experience from tests carried out with forged beam and frame structures in the development of the Saab aircraft Viggen19720022249WorkFatigue and fail-safe design features of the DC-10 airplane19720022254WorkFatigue of composites19720022259WorkFracture control procedures for aircraft structural integrity19720022260WorkThe influence of modifications of a fatigue loading history program on fatigue lifetime
No Preview Available