Advanced Response Surface Modeling of Ares I Roll Control Jet Aerodynamic InteractionsThe Ares I rocket uses roll control jets. These jets have aerodynamic implications as they impinge on the surface and protuberances of the vehicle. The jet interaction on the body can cause an amplification or a reduction of the rolling moment produced by the jet itself, either increasing the jet effectiveness or creating an adverse effect. A design of experiments test was planned and carried out using computation fluid dynamics, and a subsequent response surface analysis ensued on the available data to characterize the jet interaction across the ascent portion of the Ares I flight envelope. Four response surface schemes were compared including a single response surface covering the entire design space, separate sector responses that did not overlap, continuously overlapping surfaces, and recursive weighted response surfaces. These surfaces were evaluated on traditional statistical metrics as well as visual inspection. Validation of the recursive weighted response surface was performed using additionally available data at off-design point locations.
Document ID
20100025510
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Favaregh, Noah M. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
June 28, 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NF1676L-10668Report Number: NF1676L-10668
Meeting Information
Meeting: 27th AIAA Aerodynamic Measurement and Ground Testing Conference
Location: Chicagon, IL
Country: United States
Start Date: June 28, 2010
End Date: July 1, 2010
Sponsors: American Inst. of Aeronautics and Astronautics