Aeroelastic Problems Associated With External Stories and Innovative Scaling Laws for Such Problems

reportActive / Technical Report | Accession Number: ADA388304 | Open PDF

Abstract:

This AASERT grant was initially funded 7195 and a Ph.D. student Anne Le was hired and started her studies towards a Ph. D. degree working on the problem of active control of flutter induced by stores on the wing of a typical fighter aircraft and its aeroelastic scaling. The main thrust of her research has been the development of an aeroelastic computer code capable of simulating the subsonic flutter of a fighter type wing, including stores, as well as partial span control surfaces that can be actively controlled and used for flutter suppression.

Author(s):
Friedmann, Peretz P.
Author Organization(s):
CALIFORNIA UNIV LOS ANGELES DEPT OF MECHANICAL AND AEROSPACE ENGINEERING
Descriptive Note:
Final rept. 1 Jul 1995-30 Jun 2000
Supplementary Note:
DOI: 10.21236/ADA388304
Pagination:
0003

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFRL-SR-BL-TR-01-0231
Contract/Grant Number(s):
F49620-95-1-0453
Monitor Series:
TR-01-0231, AFOSR/VA
 Subject Terms
Joint Capability Areas:
JCA_1_Force Support; JCA_1.2_Force Preparation; JCA_3.2_Engagement; JCA_3_Force Application; JCA_1.2.3_Educating; JCA_3.2.1_Kinetic Means; JCA_4.6_Engineering
Communities of Interest:
Weapons Technologies
Descriptor(s):
*AEROELASTICITY, *EXTERNAL STORES, *FLUTTER, FIGHTER AIRCRAFT, SCALING FACTOR, WINGS, AERODYNAMIC CONTROL SURFACES
Field(s)/Group(s):
Aerodynamics, Attack and Fighter Aircraft, Fluid Mechanics
Keyword(s):
PE61103D
Report Date:
2000 Jun 30
Creation Date:
2001 Apr 25