Aerodynamic Characteristics of a Wing with Unswept Quarter-Chord Line, Aspect Ratio 2, Taper Ratio 0.78, and NACA 65A004 Airfoil Section - Transonic Bump Method

reportActive / Technical Report | Accession Number: ADA801172 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Polhamus, Edward C. ; Campbell, George S.
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Descriptive Note:
Research memo.
Pagination:
0027

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-L50A18
Monitor Series:
NACA
 Subject Terms
Joint Capability Areas:
JCA_6.4.1_Secure Information Exchange; JCA_6_Net Centric; JCA_6.4_Information Assurance
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*AERODYNAMIC CHARACTERISTICS, *WINGS, TRANSONIC FLOW, AIRFOILS
Keyword(s):
ATI 72382, ATI COLLECTION
Report Date:
1950 Mar 08
Creation Date:
2010 Oct 06