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

reportActive / Technical Report | Accession Number: ADB000285 | Open PDF

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.

Author(s):
Stelma, Jerry L.
Author Organization(s):
BOEING COMMERCIAL AIRPLANE CO SEATTLE WA
Descriptive Note:
Final rept. on Phase 2, Task 5
Supplementary Note:
Report on SST Technology Follow-On Program. See also AD913365 and ADB000286
Pagination:
0061

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):
D6-60293, FAA-SS-73-16
Contract/Grant Number(s):
DOT-FA72WA-2893
Monitor Series:
73-16, FAA
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_5.3_Planning; JCA_3_Force Application; JCA_3.1.2_Maneuver to Insert; JCA_3.1_Maneuver; JCA_3.2_Engagement; JCA_3.2.1_Kinetic Means; JCA_1.2.5_Lessons Learned; JCA_JCA_4.1.2_Sustain the Force; JCA_4.1_Deployment and Distribution
Communities of Interest:
Cyber
Descriptor(s):
*FLUTTER, *HORIZONTAL STABILIZERS, *SUPERSONIC TRANSPORT AIRCRAFT, AERODYNAMIC STABILITY, AVIATION SAFETY, ELEVATING GEAR, EQUATIONS OF MOTION, FREQUENCY, HAZARDS, HYDRAULIC ACTUATORS, STIFFNESS, TAILS(AIRCRAFT), VELOCITY, WEIGHT
Field(s)/Group(s):
Aerodynamics, Transport Aircraft
Keyword(s):
*SST TECHNOLOGY FOLLOW ON PROGRAM
Report Date:
1974 Jun 01