Progress Report on Methods of Analysis Applicable to Monocoque Aircraft Structures. Air Service Information Circular, Volume 8, Number 713.

reportActive / Technical Report | Accession Number: ADA370020 | Open PDF

Abstract:

Historical study of methods of analysis applicable to the design of monocoque aircraft structures. Surveys tile rational theoretical procedures developed for, and applicable to, stiffened and unstiffened stressed skin structures to see which methods could be used in aircraft design, which could be used if modified by the introduction of empirical coefficients, and which appeared to be inapplicable regardless of how they were changed.

Author(s):
Newell, J. S. ; Harrington, J. H.
Author Organization(s):
AIR SERVICE COMMAND PATTERSON FIELD OH
Supplementary Note:
DOI: 10.21236/ADA370020
Pagination:
0050

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFRL-WS-WP-TM-1999-9010
Monitor Series:
XD
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_5.3_Planning; JCA_6.4.1_Secure Information Exchange; JCA_4.5.4_Requirements Definition; JCA_4.5_Operational Contract Support; JCA_6_Net Centric; JCA_1.2.5_Lessons Learned; JCA_6.4_Information Assurance; JCA_1_Force Support; JCA_4.6_Engineering; JCA_6.1.1_Wired Transmission; JCA_1.2_Force Preparation; JCA_5.2.2_Develop Knowledge and Situational Awareness; JCA_5.2_Understand; JCA_6.1_Information Transport; JCA_8_Building Partnerships
Communities of Interest:
Air Platforms
Descriptor(s):
*STRESSES, *STRUCTURAL ANALYSIS, *SHELLS(STRUCTURAL FORMS), *MONOCOQUES, COEFFICIENTS, HISTORY, AIRFRAMES, AIRCRAFT DESIGN
Field(s)/Group(s):
Research and Experimental Aircraft, Laminates and Composite Materials
Keyword(s):
MONOCOQUE AIRCRAFT
Report Date:
1939 May 15
Creation Date:
1999 Nov 17