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Box No.
Barcode/UNT Number
Report No.SuffixTitlePrint OCLC No.
Electr. OCLC No.
Serial Info
HT/UNT Status
HT/UNT-LinksNotes
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NavyBox003NAVORD
39015104956084492Quality control chart technique /203606031949
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NavyBox005NAVORD
390150953391261249
Supersonic lift and centers of pressure of rectangular fin assemblies in combination with a long, cylindrical body /
1268336150
4
NavyBox005NAVORD
390150953392411488Section 7
Handbook of supersonic aerodynamics. Section 7, Three-dimensional airfoils /
319435629Volume 3
5
NavyBox005NAVORD
390150953393991488Section 18
Handbook of supersonic aerodynamics : Section 18, Shock tubes /
851077787Volume 6
6
NavyBox005NAVORD
390150953391001488Section 16
Handbook of supersonic aerodynamics : Section 16, Mechanics of rarefied gases /
1268335931Volume 5
7
NavyBox005NAVORD
390150953392581488Section 20
Handbook of supersonic aerodynamics : Section 20, Wind tunnel instrumentation and operation /
1268336043Volume 6
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NavyBox004A390151049750921488
Handbook of supersonic aerodynamics : Volume 2 / Johns Hopkins University, Applied Physics Laboratory.
1293240214Volume 2
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NavyBox004A390151049750841488Section 6
Handbook of supersonic aerodynamics. Section 6, Two-dimensional airfoils /
1293240213Volume 3
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NavyBox004A390151049750761488Section 15
Handbook of supersonic aerodynamics : Section 15, Properties of gases /
1293240212Volume 5
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NavyBox004A390151049750681488Section 17
Handbook of supersonic aerodynamics : Section 17, Ducts, nozzles and diffusers /
1293240211Volume 6
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NavyBox004A390151049750501488Section 18
Handbook of supersonic aerodynamics : Section 18, Shock tubes /
1293240210Volume 6
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NavyBox003NAVORD
390151049560761488
Handbook of supersonic aerodynamics : Volume 1 /
12988997211950Volume 1
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NavyBox003NAVORD
390151049560681488
Handbook of supersonic aerodynamics : Volume 4 /
12988997221952Volume 4
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NavyBox003NAVORD
390151049560501488
Sections 13 & 14
Handbook of supersonic aerodynamics. Volume 5, Sections 13 & 14. Viscosity and heat transfer effects /
12988997231966Volume 5
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NavyBox004A390151049750431493Mathematical theory of airborne fire control /4706105
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NavyBox005NAVORD
390150953394152023Interference factors for slender finned bodies /1268336149
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NavyBox005NAVORD
390150953394072295
Virtual mass of cylinders with radial fins and of polygonal prisms /
976792873
19
NavyBox005NAVORD
390150953391182854
Surface temperature and pressure distributions on a circular cylinder in supersonic cross-flow /
977263998
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NavyBox005NAVORD
390150953392663854
Theoretical investigation of turbulent boundary layer flow with heat transfer at supersonic and hypersonic speeds /
977401464
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NavyBox005NAVORD
390150953392744022
Laminar boundary layer on a rotating cylinder in crossflow /
977063998
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NavyBox005NAVORD
390150953391344093
Static stability and Magnus characteristics of the 5-inch high capacity spinner rocket at low subsonic speeds /
1268335984
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NavyBox005NAVORD
390150953394234099
Analytical investigation of turbulent boundary layer heat transfer coefficients for supersonic and hypersonic flow /
977303993
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NavyBox005NAVORD
390150953391424112
Static stability and Magnus characteristics of a low-drag bomb at-subsonic speeds /
1268335985
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MCARDBox137
metadc1481652
4153Microcard Project
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NavyBox005NAVORD
390150953392824200
Method for calculating turbulent boundary layer development in supersonic and hypersonic nozzles including the effects of heat transfer /
1268335957
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MCARDBox137
metadc1481653
4286Microcard Project
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NavyBox005NAVORD
390150953394314329
Static stability and Magnus characteristics of the U.S. Navy 1,000 pound low-drag bomb at transonic speeds /
1268335958
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NavyBox005NAVORD
390150953394494467
Theory of stability of compressible laminar boundary layers with injection of a foreign gas /
1268335959
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NavyBox005NAVORD
390150953392904529
Heat-transfer characteristics of a hemisphere cylinder at hypersonic Mach numbers /
976817891
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NavyBox004A390151049750354629
Tschebyscheff antenna distribution, beamwidth, and gain tables /
15479110
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NavyBox004A390151049750275558
Temperatures in structures. Part I, General discussion and one-dimension, one-layer problem; analytic solutions /
1293240202Part 1
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NavyBox004A390151049750195558
Temperatures in structures. Part 2, One dimension, two- and three-layer plate problems; analytic solutions /
1293240201Part 2
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NavyBox004A390151049750015558
Temperatures in structures. Part 3, Two- and three-layer cylindrical shells; one-space variable, linear /
1293240200Part 3
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NavyBox004A390151049749965558
Temperatures in structures. Part 4, Two- and three-layer shpherical shell segments, one space variable, linear /
1293240199Part 4
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NavyBox004A390151049749885558
Temperatures in structures. Part 5, One-layer, two space variables, linear problems /
1293240198Part 5
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NavyBox004A390151049749705558
Temperatures in structures. Part 6, Two-layer, linear, one-space variable temperature time dependent /
1293240197Part 6
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NavyBox005NAVORD
390150953385575635
Low-to-high speed drag compilations for rocket test sled components /
1268336156
39
NavyBox005NAVORD
390150953385655659
Experimental investigation of the pressure distribution on axi-symmetric flat-face cone-type bodies at supersonic and hypersonic speeds /
1268336157
40
MCARDBox137
metadc1481654
5747Microcard Project
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UNTBox115UNT5748
Investigation of strain-energy absorption potential as the criterion for determining optimum reactor-vessel containment design /
8510794371245962042
http://digital.library.unt.edu/ark:/67531/metadc1536332/
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NavyBox005NAVORD
390150953385735763
Temperature recovery factors on a 40-degree cone cylinder with turbulent boundary layer at Mach numbers 4.1 and 4.8 /
1109558275
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NavyBox005NAVORD
390150953385816420
Ground interference effects on bodies moving through a compressible fluid and their applications to SNORT designs /
1268336158
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NavyBox005NAVORD
390150953387066548Thrust-vectoring experiments with gas injection /1268336159
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NavyBox005NAVORD
390150953387146661
Drag and roll coefficients at subsonic to supersonic velocities of 1/7-scale free-flights models of the 1,000 pound low-drag bomb (EX-10) /
1268336160
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NavyBox005NAVORD
390150953387226669
Heat-transfer and pressure measurements on flat-faced flared-tail circular cylinders and normal disks /
1268336161
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NavyBox005NAVORD
390150953387306683
Measurement of the characteristics of the compressible turbulent boundary layer with air injection /
851079600
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NavyBox005NAVORD
390150953388546708
Preliminary results of flow surveys about an inclined body of revolution at Mach number 3.5 : (phase I of aft-entry program) /
1268336162
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NavyBox005NAVORD
390150953388626726
Stability criteria for numerical solutions of the normal and shock regions in unsteady two-dimensional cylindrical Lagrangian flow /
851083002
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NavyBox005NAVORD
390150953388706745
Flight environment of long-range ballistic missiles and glide vehicles /
1268336163
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NavyBox005NAVORD
390150953388886866
Investigation of the flow over an axisymmetric compression surface at high Mach numbers /
1268336164
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