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Box No.Barcode/UNT NumberReport No.SuffixTitlePrint OCLC No.
Electr. OCLC No.
Serial Info
HT/UNT Status
HT/UNT-LinksNotes
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ARMYBox001BRLTR39015095328517TR-02139
Computation of transonic flow past projectiles at angle of attack /
1270975700
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ARMYBox001BRLTR39015095328525TR-02293
MC DRAG - a computer program for estimating the drag coefficients of projectiles /
1270977214
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ARMYBox001BRLTR39015095328533TR-02341Flow model for the effect of a slanted base on drag /1270977206
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ARMYBox001BRLTR39015095328541TR-02363
Numerical simulation of steady supersonic flow over an ogive cylinder boattail body /
1270977205
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ARMYBox001BRLTR39015095328558TR-02384
Computations of the magnus effect for slender bodies in supersonic flow /
1270977204
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ARMYBox001BRLTR39015095328566TR-02458
Transonic shock-turbulent boundary layer interactions on spinning axisymmetric bodies at zero angle of attack./
1270977203
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ARMYBox001BRLTR39015095328574TR-02485
Grid network generation with adaptive boundary points for projectiles at transonic speed /
1270977202
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ARMYBox001BRLTR39015095328582TR-02501
Navier-Stokes computational study of the influence of shell geometry on the magnus effect at supersonic speeds /
1270977201
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ARMYBox001BRLTR39015095328590TR-02505
Numerical modeling of rotating band flow field and comparison with experiment /
1270977200
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ARMYBox001BRLTR39015095328608TR-02521
Liquid payload roll moment induced by a spinning and coning projectile /
1270977199
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ARMYBox001BRLTR39015095328616TR-02523
Computational modeling of aerodynamic heating for XM797 nose cap configurations /
1270977198
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ARMYBox001BRLTR39015095328624TR-02525
Some aerodynamic characteristics of a projectile shape with a nonaxisymmetric boattail at Mach numbers of 0.91 and 3.02 /
1270977197
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ARMYBox001BRLTR39015095328632TR-02532
Navier-Stokes computations of projectile base flow at transonic speeds with and without base injection /
1270977195
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ARMYBox001BRLTR39015095328640TR-02643
Navier-Stokes computational study of axisymmetric transonic turbulent flows with a two-equation model of turbulence /
1270977194
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ARMYBox001BRLTR39015095342609TR-02727
Asymptotic analysis of the roots of a certain transcendental equation /
1270977193
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ARMYBox001BRLTR39015095342617TR-02775
Moment exerted on a coning projectile by a spinning liquid in a spheroidal cavity /
26617775
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ARMYBox001BRLTR39015095342625TR-03018
Assessing the accuracy of vulnerability models by comparison with vulnerability experiments /
1270975638
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ARMYBox001BRLTR39015095342633TR-03119
Supersonic/hypersonic aerodynamics and heat transfer for projectile design Using viscous-inviscid interaction /
1270975637
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