Subsonic Free-Flight Data for a Complex Asymmetric Missile

Whyte, Robert H.; Winchenbach, G. L.; Hathaway, Wayne

doi:10.2514/3.56053

Cited by 23 publications

(2 citation statements)

References 2 publications

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“…Computational fluid dynamics techniques have been applied to complex projectile aerodynamic phenomena with much success (11)(12)(13)(14). Spark ranges, in existence since the 1940s, provide extremely accurate aerodynamic coefficients (15)(16)(17) due to the free-flight nature and motion measurement accuracy of the experiment. Experimental techniques have enjoyed recent advancement with the onboard sensor technique (18).…”

Section: Introductionmentioning

confidence: 99%

Projectile Roll Dynamics and Control With a Low-Cost Skid-to-Turn Maneuver System

Fresconi¹,

Celmins²,

Ilg³

et al. 2013

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Section: Introductionmentioning

confidence: 99%

Projectile Roll Dynamics and Control With a Low-Cost Skid-to-Turn Maneuver System

Fresconi¹,

Celmins²,

Ilg³

et al. 2013

View full text Add to dashboard Cite

show abstract

“…The angular ARF. This is accomplished by using the Aeroballistic disturbances that were obtained were caused by the normal Research Facility Data Analysis System (ARFDAS) 8 shown sabot separation process. A photograph of the model/sabot in Figure 4.…”

Section: -_"mentioning

confidence: 99%