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AFFDL-TR-74-112

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Sonic Fatigue Design Guide for Military Aircraft

This report was prepared by Acoustics Vibration Associates, Atlanta, 
Georgia, a Division of Science Appl i cat ions, Inc., 
LaJol la, Cal i fornia, 
for the Aero-Acoustics Branch, Vehicle Dynamics Division, Air Force Fl ight 
Dynamics Laboratory, Wright-Patterson Air Force Base, Ohio, under Contract 
F 33615-73-C-3124. The work described herein was conducted as Air Force 
System Canmand's exploratory development program. It establishes design 
and design cri teria for sonic fatigue prevent ion for fl ight vehicles. 
This program was directed under Project 1471, I 'Aero—Acoustic Probl ems in 
Task 147101, 
"Sonic Fatigue," and Work Unit 1147101 40, 
Flight Vehicles,' 
"Sonic Fatigue Design Handbook for Mi litary Aircraft." 
Mr. R. C. W. van der Heyde was the engineer in charge Of the work. 
This report concludes the work on Contract F 33615-73-C-3124, which 
covered the period from June 1973 to August 1974. 
The authors of the report grateful ly acknowledge the ass i stance rendered 
by R. H. Burr in, C. L. Balfour, and L. Densmore in developing and reproducing 
design and figures presented in the report. Spec i al acknowledge— 
ment is given to Hrs. Peggy Weldon and Mrs. Margaret Clark for the meticu Ious 
typing of the manuscript. The Acoustics E, Vibration Associates report 
identifi cation number is AVA/ TR 73—280. 
The report was submi t ted for publ icatiOn by the authors on 28 March 
1975.

 

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AFFDL-TR-74-112

  • Version
  • 586 Downloads
  • 17.73 MB File Size
  • 1 File Count
  • March 1, 2017 Create Date
  • March 1, 2017 Last Updated
Scroll for Details

Sonic Fatigue Design Guide for Military Aircraft

This report was prepared by Acoustics Vibration Associates, Atlanta, 
Georgia, a Division of Science Appl i cat ions, Inc., 
LaJol la, Cal i fornia, 
for the Aero-Acoustics Branch, Vehicle Dynamics Division, Air Force Fl ight 
Dynamics Laboratory, Wright-Patterson Air Force Base, Ohio, under Contract 
F 33615-73-C-3124. The work described herein was conducted as Air Force 
System Canmand's exploratory development program. It establishes design 
and design cri teria for sonic fatigue prevent ion for fl ight vehicles. 
This program was directed under Project 1471, I 'Aero—Acoustic Probl ems in 
Task 147101, 
"Sonic Fatigue," and Work Unit 1147101 40, 
Flight Vehicles,' 
"Sonic Fatigue Design Handbook for Mi litary Aircraft." 
Mr. R. C. W. van der Heyde was the engineer in charge Of the work. 
This report concludes the work on Contract F 33615-73-C-3124, which 
covered the period from June 1973 to August 1974. 
The authors of the report grateful ly acknowledge the ass i stance rendered 
by R. H. Burr in, C. L. Balfour, and L. Densmore in developing and reproducing 
design and figures presented in the report. Spec i al acknowledge— 
ment is given to Hrs. Peggy Weldon and Mrs. Margaret Clark for the meticu Ious 
typing of the manuscript. The Acoustics E, Vibration Associates report 
identifi cation number is AVA/ TR 73—280. 
The report was submi t ted for publ icatiOn by the authors on 28 March 
1975.

 

FileAction
AFFDL-TR-74-112 Sonic Fatigue Design Guide for Military Aircraft.pdfDownload 
17,005 Documents in our Technical Library
2458590 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...