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Accession Number:
AD0876612
Title:
Subsonic Lifting-Surface Theory Aerodynamics and Flutter Analysis of Interfering Wing/Horizontal-Tail Configurations. Part II. Wing/Tail Flutter Correlation Study.
Corporate Author:
NORTHROP CORP HAWTHORNE CA AIRCRAFT DIV
Report Date:
1970-09-01
Descriptive Note:
Final technical rept. Sep 68-Mar 70,
Pages:
0152
Contract Number:
F33615-69-C-1008
File Size:
0.00MB
