EFFECT OF LEADING-EDGE DROOP ON THE AERODYNAMIC AND LOADING CHARACTERISTICS OF A 4-PERCENT-THICK UNSWEPT-WING-FUSELAGE COMBINATION AT TRANSONIC SPEEDS

reportActive / Technical Report | Accession Number: AD0094328 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Schmeer, James W.
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC
Pagination:
0065

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-L56C14
Monitor Series:
NACA
 Subject Terms
Joint Capability Areas:
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_6.4.1_Secure Information Exchange; JCA_6_Net Centric; JCA_5.3_Planning; JCA_5_Command and Control; JCA_6.4_Information Assurance
Communities of Interest:
Air Platforms
Descriptor(s):
*WINGS, *FUSELAGES, TRANSONIC CHARACTERISTICS, LOAD DISTRIBUTION, AERODYNAMIC CHARACTERISTICS
Field(s)/Group(s):
Aircraft
Report Date:
1956 May 23