A Simple Method for Calculating the Span and Chordwise Loading on Straight and Swept Wings of any Given Aspect Ratio at Subsonic Speeds.

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Abstract:

No Abstract Identified

Author(s):
Kuchemann, D.
Author Organization(s):
AERONAUTICAL RESEARCH COUNCIL LONDON (ENGLAND)
Descriptive Note:
Technical rept.,
Pagination:
0053

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
ARC-R/M-2935, ARC-TR-15633
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*AERODYNAMIC LOADING, SWEPT WINGS, ASPECT RATIO, SUBSONIC FLIGHT, AIRFOILS, PRESSURE DISTRIBUTION, UNITED KINGDOM
Field(s)/Group(s):
Aircraft, Fluid Mechanics
Keyword(s):
U A reports, Unswept wings
Report Date:
1952 Aug 01