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Box No.Barcode/UNT NumberReport No.SuffixTitlePrint OCLC No.Electr. OCLC No.Serial InfoHT/UNT StatusHT/UNT-LinksNotes
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DOEBox020NSWC3901509524713975-037Integral approach to transient heat-conduction problems with phase transition /2273863051091188674Available HT 7/28/2021; NOT ON HT 10/24/2019, https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247139
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DOEBox020NSWC3901509524684275-045Vol 1Handbook of inviscid sphere-cone flow fields and pressure distributions /35666491103316605Available HT 7/28/2021; NOT ON HT 10/24/2019, https://babel.hathitrust.org/cgi/pt?id=mdp.39015095246842
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DOEBox020NSWC3901509524699075-045Vol 2Handbook of inviscid sphere-cone flow fields and pressure distributions /35666491103316605
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095246990
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DOEBox020NSWC3901509524714775-053Shock-tube diagnostics utilizing laser raman spectroscopy /10595213691103317119
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247147
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DOEBox020NSWC3901509524685975-062Use of phase-change paints to study fin-body interference heating /10595213711103316804
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095246859
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DOEBox020NSWC3901509524700675-063Experimental investigation of a fin-cone interference flow field at Mach 5 /10595213721103319399Available HT 7/28/2021; NOT ON HT 10/24/2019, https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247006
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DOEBox020NSWC3901509524715475-066Experimental study of forces and moments on circular bodies at high angle of attack /2273952001102776087
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247154
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DOEBox020NSWC3901509524686775-084Investigation of the damping in pitch characteristics of a ten degree cone /10595213731103314684
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095246867
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DOEBox020NSWC3901509524701475-174Two-component force balance for measuring skin friction and side force /2274050981103314652
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247014
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DOEBox020NSWC3901509524716275-176Induced side forces on bodies of revolution at high angle of attack /10595213741091072544
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247162
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DOEBox020NSWC3901509524687575-195Normal impingement of a supersonic jet on a plane : a basic study of shock-interference heating /10595213481103216430Available HT 7/28/2021; NOT ON HT 10/24/2019, https://babel.hathitrust.org/cgi/pt?id=mdp.39015095246875
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DOEBox020NSWC3901509524702276-026Static multiple-load measurement technique as utilized in the Naval Surface Weapons Center's wind tunnels /2274238751103318450
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247022
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DOEBox020NSWC3901509524717076-071Boundary-layer transition experiments on pre-ablated graphite nosetips in a hyperballistics range /10595212051103316855
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247170
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DOEBox020NSWC3901509524688376-121Effect of nose diameter on the erosion of spherical nosetip reentry bodies /10595212061102007303
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095246883
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DOEBox020NSWC3901509524703077-007Temperature-step effects on direct measurement of skin-friction drag /2274869601091065548
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247030
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DOEBox020NSWC3901509524718877-016Prediction of impact pressures, forces, and moments during vertical and oblique water entry /2274611121102008043
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247188
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DOEBox020NSWC3901509524689177-028Program for computing steady inviscid three-dimensional supersonic flow on reentry vehicles : volume I : analysis and programming /2274581641103318959
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095246891
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DOEBox020NSWC3901509524704877-032Program for computing steady inviscid three-dimensional supersonic flow on reentry vehicles : volume II - users manual /2274687901102687712
Available HT 7/28/2021; NOT ON HT 10/24/2019
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095247048
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NavyBox002NSWC-TR3901509533980377-059
Boundary-layer transition experiments on sharp, slender cones in supersonic freeflight /
1280153162
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NavyBox002NSWC-TR3901509533979579-153
Influence of roughness and blowing on compressible turbulent boundary layer flow /
1280153161
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NavyBox002NSWC-TR3901509533964779-416
Influence of roll orientation-dependent aerodynamics on the stability of cruciform missile configurations /
9480942
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NavyBox002NSWC-TR3901509533942880-208
Optimal bodies for minimum total drag at supersonic speeds /
6822273
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NavyBox002NSWC-TR3901509533978780-243
Correlation of instantaneous impact drag coefficients for vertical water entry /
1280153160
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NavyBox002NSWC-TR3901510495494980-346Part I
Aerodynamics of tactical weapons to Mach number 8 and angle of attack 180°. Part I, Theory and application /
1280153159
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NavyBox002NSWC-TR3901509533976180-358Part II
Aerodynamics of tactical weapons to Mach number 8 and angle of attack 180°. Part II, Computer program and users guide /
1280153158
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NavyBox002NSWC-TR3901509533975382-286
Calculations of flowfield about indented nosetips /
1280153157
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NavyBox002NSWC-TR3901509533963982-394
Vortex asymmetry development on a tangent ogive /
1280153156
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NavyBox002NSWC-TR3901509533962183-428
Inviscid computational method for supersonic inlets /
1280153155
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NavyBox002NSWC-TR3901509533961383-468
Computation and comparison with experimental data of the STD/ARM aerodynamic coefficients /
1280153154
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NavyBox002NSWC-TR3901509533960584-484
Generation of the starting plane flowfield for supersonic flow over a spherically capped body /
1280153153
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NavyBox002NSWC-TR3901509533948085-484
Multiple zone method for supersonic tactical missiles /
1280153152
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NavyBox002NSWC-TR3901509533947286-253
Nonaxisymmetric body, supersonic, aerodynamic prediction /
1280153050
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NavyBox002NSWC-TR3901509533946486-286
Numerical analysis of terminal double mach reflection /
1280153049
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NavyBox002NSWC-TR3901509533945686-342
Leeside crossflow modeling in Euler space-marching computations /
1280153151
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NavyBox002NSWC-TR3901510495491586-506
Second order Godunov method for supersonic tactical missiles /
1162849514
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NavyBox002NSWC-TR3901510495492389-099
Nonaxisymmetric body, supersonic, inviscid dynamic derivative prediction /
1280153150
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NavyBox002NSWC-TR3901510495493190-683
Second-order shock-expansion theory extended to include real gas effects /
1280153058
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NavyBox001NSWCTR3801509534006691-086Zeus user manual "real gas" effects 1285306009
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