THEORETICAL WEIGHT-FORMULA OF TAPERED WINGS,

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Abstract:

Discussions are presented on 1 Weight of spar flanges 2 weight of longeron spar webs 3 effect of sweep-back of wing 4 statistical correction factors to theoretical weight formulas of longeron flanges and webs and 5 weight of other wing-elements and weight formula for entire wing.

Author(s):
Fadeev, N. N.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Metody Priblizhennykh Raschetov i Vybora Parametrov pri Proektirovanii Samoletov, unedited rough draft trans. of Aviatsionnyi Institut, Moscow. Trudy (USSR) 1961, v. 138, p. 28-47. Another trans. is available from CFSTI or SLA $9.60 in FTD-TT-62-451, AD-287 668, 7 Sep 62, 116p.
Annotation:
Translation of Russian research: Theoretical weightformula of tapered wings.
Pagination:
0026

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-TT-64-802, TT-65-61672
Monitor Series:
65-61672
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*WEIGHT, TAPER, WINGS, STATISTICAL ANALYSIS, LOAD DISTRIBUTION, FLANGES, AIRCRAFT, STRUCTURAL COMPONENTS, USSR
Report Date:
1965 Feb 02