Author: Eugene C. Naumann
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 36
Book Description
Axial-load Fatigue Tests Using Loading Schedules Based on Maneuver-load Statistics
Author: Eugene C. Naumann
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 36
Book Description
Axial-load Fatigue Tests Using Loading Schedules Based on Maneuver-load Statistics
Author: Eugene C. Naumann
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 0
Book Description
Axial-load Fatigue Tests Using Loading Schedules Based on Maneuver-load Statistics
Author: Eugene C. Naumann
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 30
Book Description
Axial-load Fatigue Tests Using Loading Schedules Based on Maneuver-load Statitics
Influence of Programing Techniques and of Varying Limit Load Factors on Maneuver Load Fatigue Test Results
Author: Patrick L. Corbin
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 26
Book Description
Variable-amplitude axial-load fatigue tests were conducted on 7075-T6 aluminum-alloy edge-notched specimens having a theoretical elastic stress concentration factor of 4. The load programs were designed to approximate maneuver load spectra. Fatigue life was found to be shorter for random form tests than for block form tests having the same load spectrum. The greatest change in life occurred when the test program contained negative loads. Life for variable-amplitude tests was found to increase as much as 60 percent above the original test life after preloading with a program having a higher limit load factor. The summations of cycle ratios were approximately 2 for tests without negative loads but were approximately 1 for tests with negative loads.
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 26
Book Description
Variable-amplitude axial-load fatigue tests were conducted on 7075-T6 aluminum-alloy edge-notched specimens having a theoretical elastic stress concentration factor of 4. The load programs were designed to approximate maneuver load spectra. Fatigue life was found to be shorter for random form tests than for block form tests having the same load spectrum. The greatest change in life occurred when the test program contained negative loads. Life for variable-amplitude tests was found to increase as much as 60 percent above the original test life after preloading with a program having a higher limit load factor. The summations of cycle ratios were approximately 2 for tests without negative loads but were approximately 1 for tests with negative loads.
Variable-amplitude Fatigue Tests with Particular Attention to the Effects of High and Low Loads
Author: Eugene C. Naumann
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 32
Book Description
NASA Technical Note
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990
Book Description
Guide to Annual Subject Index for Technical Publications Announcements, Apr.-Dec. 1962
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 720
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 720
Book Description
Technical Publications Announcements with Indexes
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318
Book Description