Accession Number:

ADB000285

Title:

Flutter Analysis of an All-Movable Horizontal Tail with Geared Elevator on a Supersonic Transport

Descriptive Note:

Final rept. on Phase 2, Task 5

Corporate Author:

BOEING COMMERCIAL AIRPLANE CO SEATTLE WA

Personal Author(s):

Report Date:

1974-06-01

Pagination or Media Count:

61.0

Abstract:

This document presents symmetric flutter analyses conducted on the all-movable horizontal tail of the Boeing-designed SST. Interaction effects on flutter speed that are produced by the wing, fuselage, control systems and elevator gear ratio are included. Failure conditions of the horizontal-tail actuators are covered.

Subject Categories:

  • Aerodynamics
  • Transport Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE