Mechanical Actuators for Guidance of a Supersonic ... - CFD4Aircraft

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700 ft Range Tests – Divert DemonstrationAim PointSeries of yaw cards show that projectile is clearly divingdown due to pins deployed after launch.Authorized for public release. Distribution Unlimited.06/21/2007 28
Transonic Spark Photograph Layout• 5 groups of 5 stations• Each Station provides Shadowgraphs for Vertical Plane – Wall Horizontal Plane - PitProjectileShadowgraphGroup 1 Group 2 Group 3 Group 4 Group 53 mNominal Pin Deployment39.5 m 45.8 m162 mAuthorized for public release. Distribution Unlimited.06/21/2007 29
Page 4 and 5: Guided bullets to intercept mortars
Page 6 and 7: Concept of implementing flow contro
Page 10 and 11: Parametric Study DetailsPin locatio
Page 12 and 13: Effect of Separation Distance (betw
Page 14 and 15: Mach 2.5 Experiments at GTRI½ Proj
Page 16 and 17: Second Generation Actuator Rotates
Page 18 and 19: Using CFD to Predict Range Test Res
Page 20 and 21: ARL Range Test Setup• 6 Orthogona
Page 22 and 23: Shadowgraphs from Range - Count Rot
Page 24 and 25: What went wrong?• Compromises in
Page 26 and 27: 700 ft Range Preliminary Tests• O
Page 30 and 31: Divert Demonstrated by Shadowgraphs
Page 32: Conclusions• A demonstration of s

Mechanical Actuators for Guidance of a Supersonic ... - CFD4Aircraft

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