Stress Analysis of Outer Wing Bulkheads and Auxiliary Spar - Model XB-36

Vaughan, J. R.

Stress Analysis of Outer Wing Bulkheads and Auxiliary Spar - Model XB-36

Active / Technical Report | Accession Number: ADB812170 | Open PDF

Abstract:

A stress analysis is made of the outer wing bulkheads and auxiliary spar of the XB-36 bomber. The analysis covers the inter-spar and trailing edge bulkheads Nos. 29 and 30, a typical air load nose rib, and a typical portion of the wing auxiliary spar. A summary of the critical margins of safety is included.

Author(s):

Vaughan, J. R.

Author Organization(s):

GENERAL DYNAMICS CORP FORT WORTH TX

Supplementary Note:

PDF updated 22 May 2013. DOI: 10.21236/ADB812170

Pagination:

0015

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release, Document Partially Illegible

Distribution Statement:

Approved For Public Release; Distribution Is Unlimited. Document Partially Illegible.

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

FZS-36-242A

Contract/Grant Number(s):

W535-AC-22352

Monitor Series:

USAF

Subject Terms

Joint Capability Areas:

JCA_5_Command and Control; JCA_5.3_Planning

Modernization Areas:

Directed Energy

Communities of Interest:

Air Platforms

Descriptor(s):

*STRESS ANALYSIS, *WINGS, AERODYNAMIC LOADING, BOMBER AIRCRAFT, BULKHEADS, NOSES, RIBS, TRAILING EDGES

Field(s)/Group(s):

Bombers

Keyword(s):

ATI 53462, ATI COLLECTION XB 36 AIRCRAFT

Report Date:

1948 May 01

Creation Date:

1999 Jan 06