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May 8, 2006                                            Volume 3, Number 10

 

Aerodynamics Lab tests contract-winning SDB II

The Aerodynamics Laboratory at the National Institute for Aviation Research recently performed wind tunnel tests for the Raytheon Small Diameter Bomb (SDB) II.

 

In April, Raytheon was awarded a $144 million contract from the U.S. Air Force Air Armament Center, Eglin Air Force Base, Fla., to conduct risk reduction work for the for SDB II.

 

The SDB II is a netted weapon with an all-weather tri-mode seeker that provides warfighters with advanced capability to attack moving targets. This results in a robust weapon system compatible with a wide variety of GPS-based targeting systems that can acquire and recognize moving targets.

                         

Raytheon will be competing for selection in 42 months as the prime contractor for the SDB II program, which has a potential value of more than $1.3 billion.

 

Raytheon engineers spent more than 120 hours in the seven foot by ten foot Walter H. Beech Wind Tunnel testing the aerodynamic effects and perfecting the design of the SDB II.

 

Wind tunnel model of the Raytheon Small Diameter Bomb (SDB) II. The endplates were used for mounting purposes only and are not part of the SDB II design.

 

Mounting the SDB II proposed a challenge because it was necessary to see the aerodynamic effects on the fuselage without it being affected by a mounting device. To solve this problem, endplates were attached to the wind section in order to mount the model. The aerodynamics effects of the endplates were then subtracted from the final result.

 

“This approach allowed us to measure 52 pressures on the afterbodies and the bases over a wide range of angle of attack, with negligible effects from the model-support system,” said Raytheon Missile Systems Engineering Fellow David R. Carlson.

 

According to Raytheon test engineers, the wind tunnel data collected during this test may be the most comprehensive database for base and boattail pressures in the presence of deflected and undeflected control surfaces that has ever been acquired by any organization.

 

NIAR’s Aerodynamics Lab centers around the recently modernized Walter H. Beech Memorial Wind Tunnel, a premier low-speed, closed return wind tunnel.  The lab also includes a flow visualization tunnel, and has access to the WSU College of Engineering’s 3x4-foot subsonic wind tunnel and two super-sonic wind tunnels. To learn more visit www.aero-labs.org.

 
 






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