Aerodynamic Characteristics of a Wing with Unswept Quarter-Chord Line, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A004 Airfoil Section - Transonic-Bump Method

reportActive / Technical Report | Accession Number: ADA801299 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Myers, Ii, Boyd C. ; Wiggins, James W.
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Descriptive Note:
Research memo.
Pagination:
0037

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
NACA-RM-L50C18
Monitor Series:
NACA
 Subject Terms
Joint Capability Areas:
JCA_5.3_Planning; JCA_5_Command and Control
Modernization Areas:
Cyber
Communities of Interest:
Air Platforms
Descriptor(s):
*WINGS, AERODYNAMIC CHARACTERISTICS, TRANSONIC FLOW, AIRFOILS, WIND TUNNEL TESTS
Keyword(s):
ATI 75595, ATI COLLECTION
Report Date:
1950 May 08
Creation Date:
2010 Nov 17