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High Speed Research (HSR) Multi-Year Summary Report for Calendar Years 1995-1999The Aeroelasticity Task is intended to provide demonstrated technology readiness to predict and improve flutter characteristics of an HSCT configuration. This requires aerodynamic codes that are applicable to the wide range of flight regimes in which the HSCT will operate, and are suitable to provide the higher fidelity required for evaluation of aeroservoelastic coupling effects. Prediction of these characteristics will result in reduced airplane weight and risk associated with a highly flexible, low-aspect ratio supersonic airplane with narrow fuselage, relatively thin wings, and heavy engines. This Task is subdivided into three subtasks. The first subtask includes the design, fabrication, and testing of wind-tunnel models suitable to provide an experimental database relevant to HSCT configurations. The second subtask includes validation of candidate unsteady aerodynamic codes, applicable in the Mach and frequency ranges of interest for the HSCT, through analysis test correlation with the test data. The third subtask includes efforts to develop and enhance these codes for application to HSCT configurations. The wind tunnel models designed and constructed during this program furnished data which were useful for the analysis test correlation work but there were shortcomings. There was initial uncertainty in the proper tunnel configuration for testing, there was a need for higher quality measured model geometry, and there was a need for better measured model displacements in the test data. One of the models exhibited changes in its dynamic characteristics during testing. Model design efforts were hampered by a need for more and earlier analysis support and better knowledge of material properties. Success of the analysis test correlation work was somewhat muted by the uncertainties in the wind tunnel model data. The planned extent of the test data was not achieved, partly due to the delays in the model design and fabrication which could not be extended due to termination of the HSR program.
Document ID
20110022353
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Baker, Myles
(Boeing Phantom Works Hampton, VA, United States)
Boyd, William
(Boeing Phantom Works Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
September 30, 1999
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-13589
Report Number: NF1676L-13589
Funding Number(s)
WBS: WBS 561581.02.08.07.15.18
CONTRACT_GRANT: NAS1-20220
Distribution Limits
Public
Copyright
Public Use Permitted.
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