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 | AA | |
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1 | 53- | Barcode | Report No. | Suffix | Title | Print OCLC No. | Electr. OCLC No. | Serial Info | HT/UNT Status | HT/UNT-Links | Notes | ||||||||||||||||
2 | ASD-TRBox008WADCTN | 39015095336759 | 53-008 | Aerodynamic coefficients of thin lifting airfoils at high subsonic speeds / | 30843793 | ||||||||||||||||||||||
3 | WADC-TN-Box001A | 39015095330505 | 53-012 | Manipulability of rotary controls as a function of know diamter and control orientation / | 1203909202 | ||||||||||||||||||||||
4 | WADC-TN-Box001A | 39015095330646 | 53-038 | Survey of pilots' opinions of the C-97 flight simulator / | 1203909244 | ||||||||||||||||||||||
5 | WADC-TN-Box001A | 39015095330794 | 53-071 | Interior color schemes for aircraft gray instrument panel / | 1203909245 | ||||||||||||||||||||||
6 | WADC-TN-Box001A | 39015095330653 | 55-039 | Axially symmetric mixing of two laminar incompressible streams : II. / | 213865097 | ||||||||||||||||||||||
7 | WADC-TN-Box001A | 39015095330497 | 55-064 | Preliminary experiments on the simulation of gusts in a wind tunnel / | 213819522 | ||||||||||||||||||||||
8 | WADC-TN-Box001A | 39015095330513 | 55-194 | Four-channel noise source / | 70665026 | ||||||||||||||||||||||
9 | WADC-TN-Box001A | 39015095330802 | 55-204 | Influence of viewing distance in making settings on a linear scale / | 70319622 | ||||||||||||||||||||||
10 | WADC-TN-Box001A | 39015095330521 | 55-218 | Mechanical resistance in breathing systems : a theoretical analysis / | 1203909203 | ||||||||||||||||||||||
11 | WADC-TN-Box001A | 39015095330661 | 55-318 | Use of helium for cooling nozzles exposed to high temperature gas streams / | 213811838 | 1341498980 | Available HT 10/20/22 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095330661 | |||||||||||||||||||
12 | WADC-TN-Box001A | 39015095330679 | 55-355 | Criteria for short time exposure of personnel to high intensity jet aricraft noise / | 1203909102 | 1341498691 | Available HT 10/20/22 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095330679 | |||||||||||||||||||
13 | WADC-TR-Box010 | 39015095331941 | 55-362 | Comparisons of a single operator's performance with team performance on a tracking task / | 999728621 | ||||||||||||||||||||||
14 | WADC-TN-Box001A | 39015095330828 | 55-516 | Sensitive weighing device / | 1203909204 | 1341499021 | Available HT 10/20/22 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095330828 | |||||||||||||||||||
15 | WADC-TN-Box001A | 39015095330810 | 55-522 | Quantitative study of evaporation from the human body during short exposures to various temperatures, humidities, pressures and mass velocities / | 70321374 | 1341498717 | Available HT 10/20/22 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095330810 | |||||||||||||||||||
16 | WADC-TN-Box001A | 39015095330539 | 55-694 | High temperature-pressure air heater : (suitable for intermittent hypersonic wind-tunnel operation) / | 784946245 | 1341498915 | Available HT 10/20/22 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095330539 | |||||||||||||||||||
17 | WADC-TN-Box001A | 39015095330687 | 55-695 | Development of the Polytechnic Institute of Brooklyn hypersonic facility : (an interim report on Contract AF 33(616)-17 for the period 15 January 1952 to 31 July 1955) / | 786165315 | 1341498747 | Available HT 10/20/22 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095330687 | |||||||||||||||||||
18 | WADC-TN-Box001A | 39015095330836 | 55-744 | Prediction of critical events in contexts of different numbers of alternative events / | 70321307 | 1343852537 | Available HT 10/20/22 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095330836 | |||||||||||||||||||
19 | WADC-TN-Box001A | 39015095330547 | 55-745 | Rate of handling information and the rate of information presentation / | 1000312729 | 1341499033 | Available HT 10/20/22 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095330547 | |||||||||||||||||||
20 | WADC-TN-Box001A | 39015095330554 | 56-263 | Noise transmission from boundary layer pressure fluctuations / | 191886063 | ||||||||||||||||||||||
21 | WADC-TN-Box001A | 39015095330695 | 56-270 | Thermal buckling / | 191886144 | ||||||||||||||||||||||
22 | WADC-TN-Box001A | 39015095330786 | 56-294 | Note on the flow fields on the rear part of blunt bodies in hypersonic flow / | 191886847 | ||||||||||||||||||||||
23 | WADC-TN-Box001A | 39015095330703 | 56-297 | Local vascular response to vibrations / | 191887250 | ||||||||||||||||||||||
24 | WADC-TN-Box001A | 39015095330844 | 56-315 | Model instrumentation techniques for heat transfer and force measurements in a hypersonic shock tunnel / | 191887276 | ||||||||||||||||||||||
25 | WADC-TN-Box001A | 39015095330166 | 56-360 | Part XII | Aerodynamic studies : the forces acting on an air vehicle; a review of the literature / | 191907517 | |||||||||||||||||||||
26 | WADC-TN-Box001A | 39015095330174 | 56-360 | Part XIII | Aerodynamic studies : the forces acting on an air vehicle; a review of the literature / | 191907540 | |||||||||||||||||||||
27 | WADC-TN-Box001A | 39015095330182 | 56-360 | Part XIV | Aerodynamic studies : the forces acting on an air vehicle; a review of the literature / | 191907557 | |||||||||||||||||||||
28 | WADC-TN-Box001A | 39015095330307 | 56-360 | Part XV | Aerodynamic studies : the forces acting on an air vehicle; a review of the literature / | 191907576 | |||||||||||||||||||||
29 | WADC-TN-Box001A | 39015095330315 | 56-360 | Part XVI | Aerodynamic studies : the forces acting on an air vehicle; a review of the literature / | 191907625 | |||||||||||||||||||||
30 | WADC-TN-Box001A | 39015095330323 | 56-360 | Part XX | Aerodynamic studies : the forces acting on an air vehicle; a review of the literature / | 1203909205 | |||||||||||||||||||||
31 | WADC-TN-Box001A | 39015095330331 | 56-360 | Part XXI | Aerodynamic studies : the forces acting on an air vehicle; a review of the literature / | 191907853 | |||||||||||||||||||||
32 | WADC-TN-Box001A | 39015095330190 | 56-360 | Part XXIV | Aerodynamic studies : the forces acting on an air vehicle; a review of the literature / | 191914972 | |||||||||||||||||||||
33 | WADC-TN-Box001A | 39015095330851 | 56-395 | Inviscid flow in the stagnation point region of very blunt-nosed bodies at hypersonic flight speeds / | 48406576 | ||||||||||||||||||||||
34 | WADC-TN-Box001A | 39015095330562 | 56-397 | Skin resistance changes during acceleration / | 191916324 | ||||||||||||||||||||||
35 | WADC-TN-Box001A | 39015095330711 | 56-410 | Method for estimating damping derivatives of VTOL aircraft in transition and hovering flight / | 1203909283 | ||||||||||||||||||||||
36 | WADC-TN-Box001A | 39015095330869 | 56-485 | Comparison of four methods of encoding elevation information with complex line-inclination symbols / | 191953859 | ||||||||||||||||||||||
37 | WADC-TN-Box001A | 39015095330570 | 56-496 | Conditions near a sonic line in rotational flow / | 48587487 | ||||||||||||||||||||||
38 | WADC-TN-Box001A | 39015095330729 | 56-497 | Inversion of the Prandtl-Meyer relation for specific heat ratios of 5/3 and 5/4 / | 48587488 | ||||||||||||||||||||||
39 | WADC-TN-Box001A | 39015095330877 | 56-499 | Four-place logarithms to the Base 2 of three-digit numbers / | 191956511 | ||||||||||||||||||||||
40 | WADC-TN-Box001A | 39015095330596 | 56-541 | Reaction of ten radar air traffic controllers to operational use of the Telex twin-microphone, boom-type, split headset / | 1203909214 | ||||||||||||||||||||||
41 | WADC-TN-Box001A | 39015095330588 | 56-542 | Reaction of six radar air traffic controllers to conference control of targets simulated on a 19-inch horizontal display / | 191956826 | ||||||||||||||||||||||
42 | WADC-TN-Box001A | 39015095330737 | 57-072 | Evaluation of several hypersonic turbulent heat transfer analyses by comparison with experimental data | 15543440 | ||||||||||||||||||||||
43 | WADC-TN-Box001A | 39015095330745 | 57-095 | Heat transfer to surfaces in the neighborhood of protuberances in hypersonic flow / | 191961733 | ||||||||||||||||||||||
44 | WADC-TN-Box001A | 39015095330885 | 57-213 | Wave propagation and the method of characteristics in reacting gas mixtures with applications to hypersonic flow / | 12338227 | ||||||||||||||||||||||
45 | WADC-TN-Box001A | 39015095330893 | 57-214 | Analytic extension of the shock-expansion method / | 48587497 | ||||||||||||||||||||||
46 | WADC-TN-Box001A | 39015095330018 | 57-234 | Multiple psychophysiologic measures during gradual onset acceleration / | 192001559 | ||||||||||||||||||||||
47 | WADC-TN-Box001A | 39015095330026 | 57-236 | Some heat conduction solutions involved in transient heat transfer measurements / | 192003135 | ||||||||||||||||||||||
48 | WADC-TR-Box010 | 39015095332238 | 57-260 | Shape coding of aircraft instrument zone markings / | 192008358 | ||||||||||||||||||||||
49 | WADC-TN-Box001A | 39015095330034 | 57-264 | Theoretical analysis of a new type of heater for an intermittent hypersonic wind tunnel / | 192008603 | ||||||||||||||||||||||
50 | WADC-TN-Box001A | 39015095330000 | 57-292 | On pulse shapes suitable for flight tests / | 38069231 | ||||||||||||||||||||||
51 | WADC-TN-Box001A | 39015095330042 | 57-298 | Part I | Proceedings of the ANP Spectroscopy information meeting held August 6-7 at Wright Air Development Center / | 213867961 | |||||||||||||||||||||
52 | WADC-TN-Box001A | 39015095330158 | 57-311 | Statistical evaluation of joint range data / | 8183789 | ||||||||||||||||||||||
53 | WADC-TN-Box001A | 39015095330349 | 57-349 | On the nature of the sonic line for supersonic and hypersonic flow over blunt bodies / | 48587517 | ||||||||||||||||||||||
54 | WADC-TN-Box001A | 39015095330059 | 57-352 | Human factors considerations in the design proposals for a ballistic missile unit proficiency system, | 12333559 | Negative Image | |||||||||||||||||||||
55 | ASD-TRBox008WADCTN | 39015095337641 | 57-353 | Influence of graded impedance to tracheal air flow on timed vital capacity measurements of normal human subjects / | 192072355 | ||||||||||||||||||||||
56 | ASD-TRBox008WADCTN | 39015095337492 | 57-377 | Charts for flow parameters of helium at hypersonic speeds : Mach Number 10 to 20 / | 192073035 | ||||||||||||||||||||||
57 | WADC-TR-Box010 | 39015095332089 | 57-378 | Selective survey of French developments in flight simulators and flight instruments : I, Flight simulators / | 1226778337 | ||||||||||||||||||||||
58 | ASD-TRBox008WADCTN | 39015095337344 | 57-390 | Acoustical evaluation of F-102 production silencer / | 1139386557 | ||||||||||||||||||||||
59 | ASD-TRBox008WADCTN | 39015095337633 | 57-392 | Acoustical evaluation of two durastack ground run-up noise suppressors. / | 17430349 | ||||||||||||||||||||||
60 | ASD-TRBox008WADCTN | 39015095337484 | 57-408 | Statistical method for the extraction of stability parameters from flight-test data / | 192075417 | ||||||||||||||||||||||
61 | ASD-TRBox008WADCTN | 39015095337336 | 57-409 | Shock-wave oscillations in supersonic flow / | 192075503 | ||||||||||||||||||||||
62 | ASD-TRBox008WADCTN | 39015095337625 | 57-410 | Part I | Determination of aircraft stability coefficients from flight test data : Part 1 : Theoretical considerations / | 1139396954 | |||||||||||||||||||||
63 | ASD-TRBox008WADCTN | 39015095337476 | 57-410 | Part II | Determination of aircraft stability coefficients from flight-test data : Part 2 : Longitudinal investigations / | 1139378292 | |||||||||||||||||||||
64 | WADC-TR-Box010 | 39015095331933 | 57-424 | Radio channel load distribution analyzer for use in studies of communication flow in radar approach control centers / | 192076106 | ||||||||||||||||||||||
65 | ASD-TRBox008WADCTN | 39015095337328 | 57-427 | Effects of stress on Uropepsin excretion / | 192093742 | ||||||||||||||||||||||
66 | WADC-TR-Box010 | 39015095332220 | 57-431 | Investigation of the performance of the human monitor / | 1000052679 | ||||||||||||||||||||||
67 | WADC-TR-Box010 | 39015095332071 | 58-028 | Aircraft breathing oxygen regulator test stand calibration procedures / | 17430195 | ||||||||||||||||||||||
68 | WADC-TR-Box010 | 39015095331925 | 58-029 | Suitability of the installation of the illumination system for the experimental RAPCON center, Bldg. 206, WPAFB / | 1226778338 | ||||||||||||||||||||||
69 | WADC-TN-Box001A | 39015095329879 | 58-036 | Prediction of creativity in a sample of research scientists / | 212383785 | ||||||||||||||||||||||
70 | WADC-TR-Box010 | 39015095332212 | 58-037 | Airborne equipment for recording aircraft flight paths / | 192103998 | ||||||||||||||||||||||
71 | WADC-TN-Box001A | 39015095330067 | 58-042 | Simple passive method for predicting the path of a space ship with respect to a planet which it is approaching / | 1203909215 | ||||||||||||||||||||||
72 | WADC-TN-Box001A | 39015095330208 | 58-060 | Perceptual performance and the effective person / | 20054490 | ||||||||||||||||||||||
73 | WADC-TN-Box001A | 39015095330216 | 58-061 | Stability of personality trait rating factors obtained under diverse conditions / | 192106514 | ||||||||||||||||||||||
74 | WADC-TN-Box001A | 39015095330356 | 58-062 | Follow-up study of Naval academy graduates who entered the Air Force / | 36712467 | ||||||||||||||||||||||
75 | WADC-TN-Box001A | 39015095330364 | 58-063 | 1 | Aptitude levels in the enlisted manpower pool of the Air Force : Part I / | 193700849 | |||||||||||||||||||||
76 | WADC-TN-Box001A | 39015095330224 | 58-064 | Use of trait ratings in an assessment of 100 Air Force captains / | 1139379191 | ||||||||||||||||||||||
77 | WADC-TN-Box001A | 39015095330372 | 58-065 | Aptitude differences related to region of enlistment of basic airmen / | 50675312 | ||||||||||||||||||||||
78 | WADC-TN-Box001A | 39015095330380 | 58-066 | Survey of potential morale, motivation, and retention problems at ballistic missile sites / | 32884421 | ||||||||||||||||||||||
79 | WADC-TN-Box001A | 39015095330240 | 58-069 | Validity of the AFOQT (Form A) for prediction of student-officer success in observer training / | 192138500 | ||||||||||||||||||||||
80 | WADC-TN-Box001A | 39015095330398 | 58-082 | Some flight control problems of a circumnavigating lunar vehicle / | 1203909216 | ||||||||||||||||||||||
81 | WADC-TN-Box001A | 39015095330406 | 58-147 | Laminar heat transfer on blunt-nosed bodies in three-dimensional hypersonic flow / | 196608603 | ||||||||||||||||||||||
82 | WADC-TN-Box001A | 39015095330257 | 58-182 | Pressure and laminar heat transfer results in three-dimensional hypersonic flow / | 207117893 | ||||||||||||||||||||||
83 | WADC-TN-Box001A | 39015095330232 | 58-185 | Shroud tests of pressure and heat transfer over short afterbodies with separated wakes / | 63561518 | ||||||||||||||||||||||
84 | WADC-TN-Box001A | 39015095330075 | 58-210 | Radar mapping display simulation and performance recording device / | 1139392677 | ||||||||||||||||||||||
85 | WADC-TN-Box001A | 39015095330083 | 58-213 | Intrusion of aircraft noise into communities near two USAF air bases / | 206332233 | ||||||||||||||||||||||
86 | WADC-TN-Box001A | 39015095330091 | 58-221 | Residual masking at low frequencies / | 210242140 | ||||||||||||||||||||||
87 | WADC-TN-Box001A | 39015095330109 | 58-230 | Review of some recent developments in hypersonic flow / | 209783092 | ||||||||||||||||||||||
88 | WADC-TN-Box001A | 39015095330117 | 58-243 | Some measurements of noise reduction of air base structures / | 209717645 | ||||||||||||||||||||||
89 | WADC-TN-Box001A | 39015095330125 | 58-260 | Optimal elastic characteristics of ejection seat cushions for safety and comfort / | 1203909217 | ||||||||||||||||||||||
90 | WADC-TN-Box001A | 39015095330133 | 58-262 | Amount of information in the absolute judgment of Munsell hues / | 17430070 | ||||||||||||||||||||||
91 | AirForceBox052WADCTN | 39015104979433 | 58-263 | Series solution to the laminar heat transfer problem at hypersonic speeds / | 209612533 | ||||||||||||||||||||||
92 | WADC-TN-Box001A | 39015095330265 | 58-284 | Development of conductive cloth plantar electrode for use in measuring skin resistance / | 31806851 | ||||||||||||||||||||||
93 | WADC-TN-Box001A | 39015095330141 | 58-292 | Luminance and "expectancy" as determinants of response time to a light signal / | 1203909290 | ||||||||||||||||||||||
94 | WADC-TN-Box001A | 39015095330273 | 58-300 | Part I | Tabulation of coordinates for hypersonic axisymmetric nozzles : Part 1, Analysis and coordinates for test section Mach numbers of 8, 12 and 20 / | 207226416 | |||||||||||||||||||||
95 | WADC-TN-Box001A | 39015095330281 | 58-301 | Turbulent heat transfer on blunt-nosed bodies in two-dimensional and general three-dimensional hypersonic flow / | 207202961 | duced | |||||||||||||||||||||
96 | WADC-TN-Box001A | 39015095330299 | 58-314 | Study to determine methods of simulating g effects / | 1203909291 | ||||||||||||||||||||||
97 | WADC-TN-Box001A | 39015095330414 | 58-314 | Supplement I | Study to determine methods of simulating g effects : Supplement 1 / | 1203909078 | |||||||||||||||||||||
98 | WADC-TN-Box001A | 39015095330422 | 58-330 | (Unclassified title) : summary and status of adaptive control system program / | 1203909258 | ||||||||||||||||||||||
99 | WADC-TN-Box001A | 39015095330430 | 58-346 | Methods of analysis for space vehicle control system redundancy / | 1203909259 | ||||||||||||||||||||||
100 | WADC-TN-Box001A | 39015095330448 | 58-349 | Multi-field electronic tachistoscope / | 12333725 |