EFFECT OF LEADING-EDGE CHORD-EXTENSIONS ON THE AERODYNAMIC CHARACTERISTICS OF A 45 SWEPTBACK WING-FUSELAGE COMBINATION AT MACH NUMBERS OF 0.40 TO 1.03

reportActive / Technical Report | Accession Number: AD0006725 | Open PDF

Abstract:

No Abstract Identified

Author(s):
West, Jr., F. E. ; Liner, George ; Martz, Gladys S.
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Descriptive Note:
Reseach memo.
Pagination:
0043

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-L53B02
Monitor Series:
NACA
 Subject Terms
Joint Capability Areas:
JCA_1.1_Force Management; JCA_1_Force Support; JCA_7.2.1_Mitigate Lethal Effects; JCA_7.2_Mitigate; JCA_7_Protection; JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means; JCA_4.4.1_Food Service; JCA_4.4_Logistics Services; JCA_6_Net Centric
Communities of Interest:
Air Platforms
Descriptor(s):
*FUSELAGES, *SWEPTBACK WINGS, LEADING EDGES, STABILITY, AERODYNAMIC CHARACTERISTICS
Field(s)/Group(s):
Aircraft
Report Date:
1953 Apr 14