Free-flight range tests and numerical computations of a power-law elliptic cross-section projectile

Author:

Schuricht Paul1,Abate Gregg2,Forsythe James1,Bertin John1

Affiliation:

1. U.S. Air Force Academy, Colorado Springs, CO

2. USAF, Research Lab., Eglin AFB, FL

Publisher

American Institute of Aeronautics and Astronautics

Reference28 articles.

1. Assessment of StaticandDynamicCoefficients for theH3HypervelocityProjectile,"AIAAPaper 97-0640,Jan.1997

2. Experiment on a SupersonicVortexFlowAround aMissileBody,"Journalof Spacecraft and Rockets,Vol.29,No.3,May 1992,pp. 373-378

3. Crossflow andTurbulenceonVortexFlow Around aSupersonicMissile."Journalof Spacecraft andRockets.Vol. 35, No. 1,Jan.Feb. 1998,pp. 37-45

4. AIAApaper 2001-4319

5. Configurations atMachNumbers 0.4to 5.0,"

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