|
|
|
SEDL / STP / STP404-EB
 |
---->
STP404
Structural Fatigue in Aircraft
Rosenfeld M.
Pages: 207
Published: 1966
|
|
Table of Contents
Introduction
Rosenfeld M.
Contractual Reliability Acceptance Procedures
Coutinho J.
A New Technique for Helicopter Rotor Blade Service Life Substantiation
Amer K., Eakin J., Sullivan R.
Fatigue Failure of a Redundant Structure
Donat R., Heller R.
The Material Aspect of Reliability
Freudenthal A.
Random-Loading Fatigue Crack Growth Behavior of Some Aluminum and Titanium Alloys
Smith S.
Evaluation of Fatigue Capabilities of High-Performance Military Aircraft
Bouchard E.
Development of a Scatter Factor Applicable to Aircraft Fatigue Life
Impellizzeri L.
Fatigue Tests of Unmachined, Mechanically Machined, and Chemically Machined Panels of Aluminum and Titanium Alloys
Whaley R.
Interaction of Cyclic Torsion with Axial Loads
Ronay M.
Roll Fatigue Tests of Forged ZK60A-T5 Magnesium and 2014-T6 Aluminum Wheels
Behr R., Campbell S.
Committee: E08
Paper ID: STP404-EB
DOI: 10.1520/STP404-EB
ISBN-EB: 978-0-8031-6795-7
 ASTM International is a member of CrossRef.
0-8031-6627-3
978-0-8031-6627-1
STP404-EB
|
