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.

Descriptive Note:

Final technical rept. Sep 68-Mar 70,

Corporate Author:

NORTHROP CORP HAWTHORNE CA AIRCRAFT DIV

Personal Author(s):

Report Date:

1970-09-01

Pagination or Media Count:

152.0

Abstract:

Subject Categories:

  • Aerodynamics
  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE