Numerical Prediction of Roll Damping and Magnus Dynamic Derivatives for Finned Projectiles at Angle of Attack-Reference-Cited by-同舟云学术

Numerical Prediction of Roll Damping and Magnus Dynamic Derivatives for Finned Projectiles at Angle of Attack

Published:2012-06-25 Issue: Volume: Page:
ISSN:
Container-title:30th AIAA Applied Aerodynamics Conference
language:
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Author:

Bhagwandin Vishal¹

Affiliation:

1. Army Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2905

Reference20 articles.

1. 3Dupuis, A, "Aeroballistic Range and Wind Tunnel Tests of the Basic Finner Reference Projectile from Subsonic to High SupersonicVelocities,"TM2002-136,DefenseR&DCanadaValcartier,Oct2002

2. 4Dupuis,AD,Hathaway,W,"AeroballisticRangeTestsofthe AirForce FinnerReferenceProjectile,"TM2002-008, Defense R&DCanadaValcartier,May2002

3. 5West,KO,"ComparisonofFreeFlightSparkRangeandWindTunnelTestDataforaGenericMissileConfigurationatMach NumbersFrom0.6to2.5,"AirForceArmamentLaboratory,EglinAirForceBase,FL,AFATL-TR-81-87,Oct1981

4. 6West, K O, Whyte, R H, "Free Flight and Wind Tunnel Test of a Missile Configuration at Subsonic and Transonic Mach NumberswithAnglesofAttackupto30Degrees,"11thNavyAeroballisticSymposium,Warminster,PA,Aug1978

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