The Development of Cambered Airfoil Sections Having Favorable Lift Characteristics at Supercritical Mach Numbers

reportActive / Technical Report | Accession Number: ADA380944 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Graham, Donald J.
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MOFFETT FIELD CA AMES RESEARCHCENTER
Descriptive Note:
Technical note
Pagination:
0082

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
NACA-TN-1771
Monitor Series:
NASA
 Subject Terms
Joint Capability Areas:
JCA_4.3_Maintain; JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*AIRFOILS, SUPERCRITICAL FLOW, MACH NUMBER, LIFT
Field(s)/Group(s):
Aircraft
Keyword(s):
AQ M00 11 3622, CAMBERED
Report Date:
1948 Dec 01
Creation Date:
2000 Aug 30