Maximum Lift Coefficients of Airplanes Based on Sum of Wing and Tail Areas

reportActive / Technical Report | Accession Number: ADA801080 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Ankenbruck, Herman O.
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Descriptive Note:
Wartime rept.
Pagination:
0008

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-WR-L-556, NACA-RB-L4C31
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):
*AERODYNAMIC LIFT, TAIL ASSEMBLIES, TAILS(AIRCRAFT), WINGS, AIRCRAFT, COEFFICIENTS
Keyword(s):
ATI 7739, ATI COLLECTION
Report Date:
1944 Mar 01
Creation Date:
2010 Sep 15