Pressure-Distribution Investigation of an N.A.C.A. 0009 Airfoil with a 30-Percent-Chord Plain Flap and Three Tabs

reportActive / Technical Report | Accession Number: ADA801000 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Ames, Jr., Milton B. ; Sears, Richard I.
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Descriptive Note:
Technical note
Pagination:
0045

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-TN-759
Monitor Series:
NACA
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Communities of Interest:
Air Platforms
Descriptor(s):
*AIRFOILS, TRIM TABS, FLAPS(CONTROL SURFACES), PRESSURE DISTRIBUTION, AERODYNAMIC CHARACTERISTICS, WIND TUNNEL TESTS
Keyword(s):
ATI 7361, ATI COLLECTION
Report Date:
1940 May 01
Creation Date:
2010 Sep 15