INVESTIGATION AT HIGH SUBSONIC SPEEDS OF SOME EFFECTS OF SIDESLIP ON THE AERODYNAMIC LOADS ON FINNED AND UNFINNED BODIES MOUNTED FROM THE SWEPT-WING OF A WING-FUSELAGE MODEL

reportActive / Technical Report | Accession Number: AD0092214 | Open PDF

Abstract:

No Abstract Identified

Author(s):
King, Jr, Thomas J.
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Pagination:
0056

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-L56A24
Monitor Series:
NASA
 Subject Terms
Joint Capability Areas:
JCA_7.2.1_Mitigate Lethal Effects; JCA_7.2_Mitigate; JCA_7_Protection; JCA_3.1.1_Maneuver to Engage; JCA_3.1_Maneuver; JCA_3_Force Application; JCA_6.4.1_Secure Information Exchange; JCA_6_Net Centric; JCA_6.4_Information Assurance
Communities of Interest:
Air Platforms
Descriptor(s):
*LOAD DISTRIBUTION, *WING BODY CONFIGURATIONS, *AIRCRAFT PROTUBERANCES, *FINS, SWEPT WINGS, AERODYNAMIC LOADING, SUBSONIC FLOW, OGIVES
Field(s)/Group(s):
Aerodynamics
Report Date:
1956 Apr 26