Accession Number:

AD0744210

Title:

Acoustic Fatigue Design Data, Part 1

Descriptive Note:

AGARDograph rept.

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

• Thomson, A. G.

Report Date:

1972-05-01

Pagination or Media Count:

58.0

Abstract:

The report, the first part of a series giving data for design against acoustic fatigue, has been prepared in order to draw together the results of research in acoustic fatigue and to present them in a form directly useable in aerospace design. Future work in this series will deal with endurance of aluminum alloy and titanium alloy structures under simulated acoustic loading, stress response of flat or curved honeycomb panels, near field compressor noise estimation, stress response of box and control surface structures and structural damping.

Descriptors:

• *AIRFRAMES
• STRESSES
• NATO
• VIBRATION
• AIRCRAFT PANELS
• JET AIRCRAFT NOISE
• ACOUSTIC PROPERTIES
• FATIGUE(MECHANICS)
• RESONANT FREQUENCY
• MATHEMATICAL ANALYSIS

Subject Categories:

• Aircraft
• Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE