| A | B | C | D | E | F | G | H | I | J | K | L | M | N | O | P | Q | R | S | T | U | V | W | X | Y | Z | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
1 | Box No. | Barcode/UNT Number | Report No. | Suffix | Title | Print OCLC No. | Electr. OCLC No. | Serial Info | HT/UNT Status | HT/UNT-Links | Notes | |||||||||||||||
3 | NavyBox005NOLTR | 39015095338607 | 61-035 | Ballistics range firings for determination of drag and stability of models of Five Polaris configurations (U) / | 1267989998 | |||||||||||||||||||||
4 | DOIBox002NavyNOLTR | 39015095150010 | 61-102 | Plan to reduce costs of technical library operations in the Department of Defense / | 1012487102 | 1012487102 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150010 | ||||||||||||||||||
5 | NavyBox005NOLTR | 39015095338599 | 62-035 | Supersonic aerodynamic heat transfer and pressure distributions on a sphere-cone model at high angles of yaw / | 1013391157 | |||||||||||||||||||||
6 | DOIBox002NavyNOLTR | 39015095150028 | 62-047 | NOL hypersonic tunnel no. 4 / | 1012487101 | 1012487101 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150028 | ||||||||||||||||||
7 | NavyBox005NOLTR | 39015095338748 | 62-202 | Flow of a dilute suspension of solids in a laminar gas boundary layer / | 41484006 | |||||||||||||||||||||
8 | AECBox033NOLTR | 39015095026681 | 62-207 | Response of Enrico Fermi reactor to TNT simulated nuclear accidents / | 35469028 | 35469028 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095026681 | Available in HT 3/21/17; Not in HT 1/12/2016 | |||||||||||||||||
9 | NavyBox005NOLTR | 39015095338755 | 63-068 | On the effect of transverse curvature in compressible laminar boundary layer flow over slender bodies of revolution / | 1109555621 | |||||||||||||||||||||
10 | DOIBox002NavyNOLTR | 39015095150036 | 63-114 | NOL 3 megawatt research arc / | 1012487096 | 1012487096 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150036 | ||||||||||||||||||
11 | DOIBox002NavyNOLTR | 39015095150044 | 63-131 | Instrument for the measurement of specific volume in liquids / | 1012487095 | 1012487095 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150044 | ||||||||||||||||||
12 | NavyBox005NOLTR | 39015095338896 | 63-144 | Design and development of the Archer sounding rocket / | 1267989977 | |||||||||||||||||||||
13 | DOIBox002NavyNOLTR | 39015095150051 | 63-208 | Comparisons of experimental and theoretical heat transfer to a yawed sphere-cone model at supersonic speeds / | 669765153 | 669765153 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150051 | ||||||||||||||||||
14 | NavyBox005NOLTR | 39015095338904 | 63-224 | Comparison of equilibrium and frozen flow properties of air in a hypersonic wind tunnel / | 1109544545 | |||||||||||||||||||||
15 | NavyBox005NOLTR | 39015095338912 | 63-241 | Analytic solutions to the equations of motion of missiles having Six degrees of freedom (U) / | 1267990167 | |||||||||||||||||||||
16 | NavyBox005NOLTR | 39015095338920 | 63-261 | Laminar boundary layer calculations by finite differences / | 1267990168 | |||||||||||||||||||||
17 | UNTBox116 | UNT | 63-264 | Study of the water-entry cavity / | 20367522 | 1273560285 | http://digital.library.unt.edu/ark:/67531/metadc1536370/ | |||||||||||||||||||
18 | DOIBox002NavyNOLTR | 39015095150069 | 63-275 | Performance analysis of an AC electric arc power supply / | 1012487094 | 1012487094 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150069 | ||||||||||||||||||
19 | NavyBox005NOLTR | 39015095338763 | 63-276 | High temperature turbulent heat-transfer measurements / | 1267990174 | |||||||||||||||||||||
20 | DOIBox002NavyNOLTR | 39015095150093 | 64-041 | Charts of equilibrium real-gas stagnation point conditions on a sphere for altitudes to 200,000 feet and velocities to 15,000 feet per second / | 1012487088 | 1012487088 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150093 | ||||||||||||||||||
21 | DOIBox002NavyNOLTR | 39015095150101 | 64-065 | Air-film cooling of a supersonic nozzle / | 1012487087 | 1012487087 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150101 | ||||||||||||||||||
22 | UNTBox116 | UNT | 64-099 | Characteristics of the turbulent boundary layer with heat and mass transfer at M=6.7 / | 1273560317 | http://digital.library.unt.edu/ark:/67531/metadc1536371/ | ||||||||||||||||||||
23 | NavyBox005NOLTR | 39015095338771 | 64-116 | Stability of a towed object / | 1267990169 | |||||||||||||||||||||
24 | NavyBox005NOLTR | 39015095338615 | 64-163 | Measurements and correlation of heat transfer in a solid propellant rocket nozzle / | 30425202 | |||||||||||||||||||||
25 | NavyBox005NOLTR | 39015095338623 | 64-179 | Transmission of green laser light (5300A) through water / | 1109691648 | |||||||||||||||||||||
26 | NavyBox005NOLTR | 39015095338631 | 64-200 | Experimental Reynolds analogy factor for a compressible turbulent boundary layer with a pressure gradient / | 1109514005 | |||||||||||||||||||||
27 | NavyBox005NOLTR | 39015095338649 | 64-222 | U.S. Naval Ordnance Laboratory unclassified reports published by the Aeroballistics Abiblirea : 1 October 1945--31 December 1962 / | 1267990161 | |||||||||||||||||||||
28 | NavyBox005NOLTR | 39015095338789 | 65-008 | On the hypersonic sharp leading edge problem for bodies other than flat plates / | 30426040 | |||||||||||||||||||||
29 | NavyBox005NOLTR | 39015095338797 | 65-153 | Effect of a highly cooled wall on hypersonic turbulent heat transfer / | 1267990162 | |||||||||||||||||||||
30 | NavyBox005NOLTR | 39015095338938 | 65-226 | Effect of fluid injection on the incompressible laminar boundary layer over a slender parabola of revolution / | 1109505208 | |||||||||||||||||||||
31 | NavyBox005NOLTR | 39015095338946 | 65-241 | Bibliography of NOL technical documentation in Aeroballistics and Hydroballistics / | 1267990045 | |||||||||||||||||||||
32 | NavyBox005NOLTR | 39015095338656 | 66-054 | Laminar and turbulent boundary layers of slightly-blunted cones at hypersonic speeds / | 1267990163 | |||||||||||||||||||||
33 | NavyBox005NOLTR | 39015095339381 | 66-095 | Experimental study of the turbulent wake behind a cone at Mach 5 / | 1269074211 | |||||||||||||||||||||
34 | NavyBox005NOLTR | 39015095338664 | 66-104 | Analytical study of non-equilibrium flow in hypersonic nozzles using a simplified model for air / | 1267990164 | |||||||||||||||||||||
35 | NavyBox005NOLTR | 39015095338805 | 66-138 | Measurements of the static pressure distributions and shock shape on an oblate spheroid at Mach numbers of 3 and 6 / | 1109690558 | |||||||||||||||||||||
36 | NavyBox005NOLTR | 39015095339092 | 66-187 | Formulation of the complete equations of boundary layer stability with mass transfer / | 1109589648 | |||||||||||||||||||||
37 | DOIBox002NavyNOLTR | 39015095150077 | 66-215 | Skin friction and heat transfer characteristics of the compressible laminar boundary layer with injection of a light, medium, and heavy gas / | 1012486918 | 1012486918 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150077 | ||||||||||||||||||
38 | DOIBox002NavyNOLTR | 39015095150085 | 66-225 | Axisymmetric laminar boundary layers with very large transverse curvature / | 1012486917 | 1012486917 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150085 | ||||||||||||||||||
39 | DOIBox002NavyNOLTR | 39015095150119 | 67-024 | Measurements of hypersonic turbulent heat transfer on a highly cooled cone / | 1012487086 | 1012487086 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150119 | ||||||||||||||||||
40 | UNTBox116 | UNT | 67-027 | U.S. Naval Ordnance Laboratory hypersonic tunnel / | 1273560910 | http://digital.library.unt.edu/ark:/67531/metadc1536372/ | ||||||||||||||||||||
41 | DOIBox002NavyNOLTR | 39015095150127 | 67-032 | Mollier diagram for nitrogen / | 760964701 | 760964701 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150127 | ||||||||||||||||||
42 | DOIBox002NavyNOLTR | 39015095150135 | 67-039 | Analytical investigation of the flat plate turbulent boundary layer in compressible flow / | 1012487085 | 1012487085 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150135 | ||||||||||||||||||
43 | DOIBox002NavyNOLTR | 39015095150143 | 67-069 | Wind tunnel free-flight testing techniques for planar motion employed at the Naval Ordnance Laboratory / | 1012487084 | 1012487084 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150143 | ||||||||||||||||||
44 | DOIBox002NavyNOLTR | 39015095150150 | 67-108 | Approximate solution for compressible axisymmetric laminar boundary layers including the effects of transverse curvature / | 1012486922 | 1012486922 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150150 | ||||||||||||||||||
45 | DOIBox002NavyNOLTR | 39015095150168 | 67-123 | Wind tunnel simulation of head-on bow wave-blast wave interactions / | 1012486921 | 1012486921 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150168 | ||||||||||||||||||
46 | DOIBox002NavyNOLTR | 39015095150176 | 67-137 | Digital computer program for making comparative aerodynamic heat transfer and skin friction drag calculations / | 1012487083 | 1012487083 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150176 | ||||||||||||||||||
47 | DOIBox002NavyNOLTR | 39015095150184 | 67-148 | Multiple pressure transducer banks and their application / | 1012487082 | 1012487082 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150184 | ||||||||||||||||||
48 | NavyBox005NOLTR | 39015095338813 | 67-154 | Two techniques for simulating the interaction of a supersonic vehicle with a blast wave / | 1267990165 | |||||||||||||||||||||
49 | AECBox150 | 39015095284553 | 67-156 | Analysis of the split Hopkinson pressure bar / | 1138033930 | |||||||||||||||||||||
50 | DOIBox002NavyNOLTR | 39015095150192 | 67-182 | Experimental studies of shock-shock interactions on a 9° cone / | 1012487081 | 1012487081 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150192 | ||||||||||||||||||
51 | DOIBox002NavyNOLTR | 39015095150200 | 67-186 | Approximate method for the calculation of the reynolds analogy factor for a compressible turbulent boundary layer in a pressure gradient / | 811246215 | 811246215 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150200 | ||||||||||||||||||
52 | DOIBox002NavyNOLTR | 39015095150218 | 67-189 | Stagnation point heat transfer from a viscous nongray radiating shock layer : including the applicability of step model absorption coefficients and sensitivity to uncertainties in transport properties / | 1012487080 | 1012487080 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150218 | ||||||||||||||||||
53 | NavyBox001NOLTR | 39015095150226 | 68-003 | Drag of slightly blunted slender cones / | 1013548053 | 1013548053 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150226 | ||||||||||||||||||
54 | NavyBox001NOLTR | 39015095150234 | 68-004 | Hypersonic pitch-damping support using water-cooled ball bearings / | 1013548052 | 1013548052 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150234 | ||||||||||||||||||
55 | NavyBox001NOLTR | 39015095150242 | 68-005 | Critical review of analytical methods for estimating control forces produced by secondary injection : the two dimensional problem / | 1013548051 | 1013548051 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150242 | ||||||||||||||||||
56 | NavyBox001NOLTR | 39015095150259 | 68-019 | Solutions of the second-order boundary-layer equations for laminar incompressible flow / | 1013548050 | 1013548050 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150259 | ||||||||||||||||||
57 | NavyBox001NOLTR | 39015095150267 | 68-052 | Experimental investigation of the aerodynamic characteristics of slender hypersonic vehicles at high angles of attack / | 1013548049 | 1013548049 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150267 | ||||||||||||||||||
58 | NavyBox001NOLTR | 39015095150275 | 68-056 | Equation for rapid calculation of stagnation point radiative heat transfer : including shock layer radiative cooling and nongray self-absorption / | 1013548041 | 1013548041 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150275 | ||||||||||||||||||
59 | NavyBox001NOLTR | 39015095150283 | 68-060 | Hot-wire stagnation temperature probe / | 1013548040 | 1013548040 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150283 | ||||||||||||||||||
60 | NavyBox001NOLTR | 39015095150291 | 68-077 | Arc rotation in 4 ring AC arc heater / | 1013548039 | 1013548039 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150291 | ||||||||||||||||||
61 | NavyBox001NOLTR | 39015095150309 | 68-087 | Wind tunnel free-flight data-reduction program for either spinning or non spinning models utilizing data from a single plane / | 1013548038 | 1013548038 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150309 | ||||||||||||||||||
62 | NavyBox001NOLTR | 39015095150317 | 68-109 | 2.5-megawatt graphite heater for nitrogen gas / | 1013548037 | 1013548037 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150317 | ||||||||||||||||||
63 | NavyBox001NOLTR | 39015095150325 | 68-129 | On hypersonic blunt body flow fields obtained with a time-dependent technique / | 1013548036 | 1013548036 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150325 | ||||||||||||||||||
64 | NavyBox001NOLTR | 39015095150333 | 68-134 | Evaluation of a telemetry system for use in shock interaction experiments / | 1013548035 | 1013548035 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150333 | ||||||||||||||||||
65 | NavyBox001NOLTR | 39015095150341 | 68-143 | Slot jet interaction studies of an ogive cylinder at M[infinity] = 4 and 5 / | 1013548020 | 1013548020 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150341 | ||||||||||||||||||
66 | NavyBox001NOLTR | 39015095150358 | 68-151 | Experimental investigation of the surface Pitot probe including effects of heat transfer and compressibility / | 1013548019 | 1013548019 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150358 | ||||||||||||||||||
67 | NavyBox001NOLTR | 39015095150366 | 68-163 | Balance for measuring skin friction in the presence of ablation / | 1013548018 | 1013548018 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150366 | ||||||||||||||||||
68 | NavyBox001NOLTR | 39015095150374 | 68-172 | Supersonic wind tunnel magnus measurements of the 7-, 8-, 9- and 10-caliber Army-Navy Spinner Projectile / | 1013548017 | 1013548017 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150374 | ||||||||||||||||||
69 | NavyBox001NOLTR | 39015095150382 | 68-187 | Performance capability of the NOL hypersonic tunnel / | 1013548016 | 1013548016 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150382 | ||||||||||||||||||
70 | NavyBox001NOLTR | 39015095150390 | 68-192 | Method for determining the parameters of ordinary differential equations / | 1013548015 | 1013548015 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150390 | ||||||||||||||||||
71 | NavyBox001NOLTR | 39015095150408 | 68-195 | Roll-induced force and moment measurements of the M823 research store / | 1013548014 | 1013548014 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150408 | ||||||||||||||||||
72 | NavyBox001NOLTR | 39015095150416 | 69-022 | Exploratory theoretical investigation of the effect of longitudinal surface curvature on the turbulent boundary layer / | 1013547992 | 1013547992 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150416 | ||||||||||||||||||
73 | NavyBox001NOLTR | 39015095150424 | 69-036 | Separated flow phenomena on a slender cone at Mach 5 / | 1013548009 | 1013548009 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150424 | ||||||||||||||||||
74 | NavyBox001NOLTR | 39015095150432 | 69-047 | Generalization to turbulent boundary layers of Mangler's transformation between axisymmetric and two-dimensional laminar boundary layers / | 1013548007 | 1013548007 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150432 | ||||||||||||||||||
75 | NavyBox001NOLTR | 39015095150440 | 69-051 | Correlation of heat-transfer and skin-friction data and an experimental Reynolds analogy factor for highly cooled turbulent boundary layers at Mach 5.0 / | 1013547885 | 1013547885 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150440 | ||||||||||||||||||
76 | NavyBox001NOLTR | 39015095150457 | 69-052 | Time-dependent analysis for quasi-one-dimensional nozzle flows with vibrational and chemical nonequilibrium / | 1013547991 | 1013547991 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150457 | ||||||||||||||||||
77 | NavyBox001NOLTR | 39015095150465 | 69-056 | Balance for measuring skin friction in the presence of heat transfer / | 1013547990 | 1013547990 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150465 | ||||||||||||||||||
78 | NavyBox001NOLTR | 39015095150473 | 69-080 | How to analyze 2-D Schlieren photographs to obtain the density gradient structure of 3-D flow fields / | 1013547989 | 1013547989 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150473 | ||||||||||||||||||
79 | NavyBox001NOLTR | 39015095150481 | 69-106 | Velocity profile, skin-friction balance and heat-transfer measurements of the turbulent boundary layers at Mach 5 and zero-pressure gradient / | 1013547988 | 1013547988 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150481 | ||||||||||||||||||
80 | NavyBox001NOLTR | 39015095150499 | 69-108 | Oblique shock interaction experiments / | 1013547987 | 1013547987 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150499 | ||||||||||||||||||
81 | NavyBox001NOLTR | 39015095150507 | 69-110 | Hypersonic-turbulent boundary-layer separation over a cone-cylinder-flare configuration / | 1013547986 | 1013547986 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150507 | ||||||||||||||||||
82 | NavyBox001NOLTR | 39015095150515 | 69-122 | Investigation of substructure heating on cracked ablative heat shields / | 1013547670 | 1013547670 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150515 | ||||||||||||||||||
83 | NavyBox001NOLTR | 39015095150523 | 69-125 | Supersonic ablation studies with teflon / | 1013547669 | 1013547669 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150523 | ||||||||||||||||||
84 | NavyBox001NOLTR | 39015095150531 | 69-143 | Experimental investigation of the compressible turbulent boundary layer with a favorable pressure gradient / | 1013547668 | 1013547668 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150531 | ||||||||||||||||||
85 | NavyBox001NOLTR | 39015095150549 | 69-151 | Measurements of blast-induced transient pressures at the base of a cone in supersonic flow / | 1013547971 | 1013547971 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150549 | ||||||||||||||||||
86 | NavyBox001NOLTR | 39015095150556 | 69-187 | Experimental investigation of the flow field around a yawed cone / | 1013547969 | 1013547969 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150556 | ||||||||||||||||||
87 | NavyBox001NOLTR | 39015095150564 | 69-200 | Time-dependent quasi-one-dimensional analysis of population inversions in an expanding gas / | 220768461 | 220768461 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150564 | ||||||||||||||||||
88 | NavyBox001NOLTR | 39015095150572 | 69-212 | Computer program for the interception of a re-entry body by a ground-launched interceptor / | 1013547968 | 1013547968 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150572 | ||||||||||||||||||
89 | NavyBox001NOLTR | 39015095150580 | 70-002 | On the hypersonic flow past blunted, flat delta wings / | 1013547967 | 1013547967 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150580 | ||||||||||||||||||
90 | NavyBox001NOLTR | 39015095150598 | 70-012 | NOL four-ring three-phase ac arc heater (Mk IV) / | 1013547966 | 1013547966 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150598 | ||||||||||||||||||
91 | NavyBox005NOLTR | 39015095338953 | 70-038 | Analytical and experimental study of the dynamic response of cable systems / | 1193841 | |||||||||||||||||||||
92 | NavyBox005NOLTR | 39015095338961 | 70-044 | Wind-tunnel investigation of the aerodynamic characteristics of the Mark 7 Mod 2 bomblet dispenser (U) / | 1267990166 | |||||||||||||||||||||
93 | NavyBox001NOLTR | 39015095150606 | 70-048 | Transpiration cooling experiments near the stagnation line of a cylinder in cross flow / | 1013547965 | 1013547965 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150606 | ||||||||||||||||||
94 | NavyBox001NOLTR | 39015095150614 | 70-050 | Two-dimensional jet interaction with a mach 4 mainstream / | 1013547943 | 1013547943 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150614 | ||||||||||||||||||
95 | NavyBox001NOLTR | 39015095150622 | 70-081 | Fine-wire stagnation temperature probe / | 1013547942 | 1013547942 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150622 | ||||||||||||||||||
96 | NavyBox001NOLTR | 39015095150630 | 70-093 | Flow visualization studies of a fin protuberance partially Immersed in a turbulent boundary layer at mach 5 / | 1013547941 | 1013547941 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150630 | ||||||||||||||||||
97 | NavyBox001NOLTR | 39015095150648 | 70-103 | Equilibrium normal shock properties for vibrationally excited CO₂-N₂-He gas mixtures / | 1013547940 | 1013547940 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150648 | ||||||||||||||||||
98 | NavyBox001NOLTR | 39015095150655 | 70-148 | Calculation of laminar skin friction on a porous plate by a refined integral method / | 1013547939 | 1013547939 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150655 | ||||||||||||||||||
99 | NavyBox001NOLTR | 39015095150663 | 70-197 | Prediction of errors and the improvement of data obtained in wind-tunnel heat-transfer tests / | 1013547938 | 1013547938 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150663 | ||||||||||||||||||
100 | NavyBox001NOLTR | 39015095150671 | 70-198 | Numerical experiments associated with gas dynamic lasers / | 1013547937 | 1013547937 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150671 | ||||||||||||||||||
101 | NavyBox001NOLTR | 39015095150689 | 70-204 | Further evaluation of a telemetry system for use in shock interaction experiments / | 1013547936 | 1013547936 | Available HT 10/24/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095150689 | ||||||||||||||||||