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1 | Box | Barcode/UNT Number | Suffix | Title | Print OCLC No. | Electr. OCLC No. | Serial Info | HT/UNT Status | HT/UNT-Links | Notes | ||||||||||||||||
2 | AFWALBox002 | 39015095334929 | 79-3095 | Volume I | Advanced residual strength degradation rate modeling for advanced composite structures. Volume 1. Task I: Preliminary screening / | 429474239 | ||||||||||||||||||||
3 | AFWALBox002 | 39015095334770 | 79-3095 | Volume II | Advanced residual strength degradation rate Modeling for advanced composite structures. Volume 2. Tasks II and III / | 429472669 | ||||||||||||||||||||
4 | AFWALBox002 | 39015095334622 | 79-3095 | Volume III | Advanced residual strength degradation rate modeling for advanced composite structures. Volume 3. Appendixes to report for Tasks II and III / | 429484244 | ||||||||||||||||||||
5 | AFWALBox002 | 39015095334630 | 80-3007 | OPTIM III : a NASTRAN compatible large scale automated minimum weight design problem-users and programmers manual / | 1240441416 | |||||||||||||||||||||
6 | AFWALBox002 | 39015095334648 | 80-3017 | Computation of three-dimensional supersonic viscous flows in internal corners / | 1240441174 | |||||||||||||||||||||
7 | AFWALBox002 | 39015095334788 | 80-3018 | Response of nonlinear structural panels subjected to high intensity noise / | 429650317 | |||||||||||||||||||||
8 | AFWALBox002 | 39015095334796 | 80-3019 | Sonic fatigue design techniques for advanced composite aircraft structures : Final report / | 429642815 | |||||||||||||||||||||
9 | AFWALBox002 | 39015095334937 | 80-3027 | Development of a nozzle to improve the turning of supersonic Coanda jets / | 1240441467 | |||||||||||||||||||||
10 | AFWALBox002 | 39015095334945 | 80-3045 | Experimental investigation of the crack growth gage / | 429654085 | |||||||||||||||||||||
11 | AFWALBox002 | 39015095298959 | 80-3050 | Weapon bay cavity noise environments, data correlation and prediction for the B-1 aircraft / | 429654561 | |||||||||||||||||||||
12 | AFWALBox002 | 39015095298967 | 80-3061 | Holographic investigation of slender body vortex wakes / | 1240441468 | |||||||||||||||||||||
13 | AFWALBox002 | 39015095298975 | 80-3062 | Hypersonic boundary layer transition experiments / | 1240441469 | |||||||||||||||||||||
14 | AFWALBox002 | 39015095299106 | 80-3070 | High angle of attack missile aerodynamics at Mach numbers 0.30 to 1.5 / | 1240441500 | |||||||||||||||||||||
15 | AFWALBox 1 | 39015095307594 | 80-3071 | Vol. 5 | Aerodynamic configured missile development final report. Volume V, Phase II experimental program / | 1194593907 | ||||||||||||||||||||
16 | AFWALBox002 | 39015095299114 | 80-3071 | Volume I | Aerodynamic configured missile development : final report. Volume I, Executive Summary / | 1240441502 | ||||||||||||||||||||
17 | AFWALBox002 | 39015095299122 | 80-3071 | Volume II, Appendix A | Aerodynamic configured missile development : final report. Volume II, Appendix A, Configuration Development. Aerodynamic configured missile reference library summary / | 1240441089 | ||||||||||||||||||||
18 | AFWALBox002 | 39015095299254 | 80-3071 | Volume II, Appendix B | Aerodynamic configured missile development : final report. Volume II, Appendix B, Configuration Development. Relations between aerodynamic characteristics and performance / | 1240441090 | ||||||||||||||||||||
19 | AFWALBox002 | 39015095299262 | 80-3071 | Volume III | Aerodynamic configured missile development : final report. Volume III, Missile aerodynamic prediction rationale using the Supersonic/Hypersonic arbitrary body program / | 1240441503 | ||||||||||||||||||||
20 | AFWALBox002 | 39015095299270 | 80-3071 | Volume IV | Aerodynamic configured missile development : final report. Volume IV, Phase I experimental program / | 1240441223 | ||||||||||||||||||||
21 | AFWALBox002 | 39015095299130 | 80-3071 | Volume VI | Aerodynamic configured missile development : final report. Volume VI, Phase III experimental program / | 1240441504 | ||||||||||||||||||||
22 | UNTBox115 | UNT | 80-3071 | Volume II | Aerodynamic configured missile development : final report. Volume II, Configuration development / | 1245936725 | http://digital.library.unt.edu/ark:/67531/metadc1536329/ | |||||||||||||||||||
23 | UNTBox115 | UNT | 80-3073 | Structural design and wind tunnel testing of a forward swept fighter wing / | 1245936611 | http://digital.library.unt.edu/ark:/67531/metadc1536328/ | ||||||||||||||||||||
24 | AFWALBox 1 | 39015095307602 | 80-3084 | Advanced ejection seat for high dynamic pressure escape wind tunnel test report / | 1194593908 | |||||||||||||||||||||
25 | AFWALBox 1 | 39015095307610 | 80-3090 | Finite span effects on flap heating and effectiveness in a turbulent boundary layer / | 1194593909 | |||||||||||||||||||||
26 | AFWALBox 1 | 39015095307628 | 80-3102 | Use of strained coordinate perturbation method in transonic aeroelestic computations / | 1194593910 | |||||||||||||||||||||
27 | AFWALBox 3 | 39015095307867 | 80-3115 | Aerodynamic analysis of a fighter aircraft with a higher order paneling method / | 1195928920 | |||||||||||||||||||||
28 | AFWALBox 3 | 39015095307875 | 80-3117 | Vol. 1 | Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume I, Surface streamline tracing / | 1195928919 | ||||||||||||||||||||
29 | AFWALBox 3 | 39015095307883 | 80-3117 | Vol. 2 | Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume II, Computer graphics / | 1195927707 | ||||||||||||||||||||
30 | AFWALBox 1 | 39015095307636 | 80-3143 | Use of strained coordinate perturbation method in transonic aeroelestic computations / | 1194593911 | |||||||||||||||||||||
31 | AFWALBox002 | 39015095299288 | 80-4061 | Study to determine the effect of glass compositional variations on vibration damping properties / | 429655271 | |||||||||||||||||||||
32 | AFWALBox002 | 39015095299296 | 80-4104 | Relationship between tensile strength and flexure strength in fiber reinforced composites / | 60037128 | |||||||||||||||||||||
33 | AFWALBox002 | 39015095299148 | 80-4121 | Flexible fabrics from TaC-loaded carbon yarns / | 1240441042 | |||||||||||||||||||||
34 | AFWALBox002 | 39015095298983 | 81-2047 | Part I | Coaxial dump ramjet combustor combustion instabilities. Part I. Parametric test data / | 1240441505 | ||||||||||||||||||||
35 | AFWALBox002 | 39015095298991 | 81-2114 | Research on turbine rotor-stator aerodynamic interaction and rotor negative incidence stall / | 1240441562 | |||||||||||||||||||||
36 | AFWALBox002 | 39015095299007 | 81-3001 | Effects of fighter attack spectrum on composite fatigue life / | 429905546 | |||||||||||||||||||||
37 | AFWALBox002 | 39015095299015 | 81-3002 | High speed smoke flow visualization / | 946213694 | |||||||||||||||||||||
38 | AFWALBox002 | 39015095299155 | 81-3021 | Vortex breakdown and instability / | 1240441043 | |||||||||||||||||||||
39 | AFWALBox002 | 39015095299163 | 81-3035 | Evaluation of USSAERO and HABP computer codes for aerodynamic predictions for slender bodies / | 1240441563 | |||||||||||||||||||||
40 | AFWALBox002 | 39015095299304 | 81-3036 | Cavity oscillation in cruise missile carrier aircraft / | 429908526 | |||||||||||||||||||||
41 | AFWALBox002 | 39015095299312 | 81-3059 | Source-Doublet approach to modeling triple ejector rack store configurations and force calculations / | 1240441514 | |||||||||||||||||||||
42 | AFFDLTRBox003AFWALTR | 39015095307222 | 81-3073 | Vol. 1 | Panel optimization with integrated software (POIS). Volume 1, Panda -- interactive program for preliminary minimum weight design / | 1192562742 | ||||||||||||||||||||
43 | AFFDLTRBox003AFWALTR | 39015095307230 | 81-3073 | Vol. 2 | Panel optimization with integrated software (POIS). Volume 2, User instructions -- Echo and RRSYS / | 1192562741 | ||||||||||||||||||||
44 | AFFDLTRBox003AFWALTR | 39015095307248 | 81-3079 | Handbook of force management methods / | 780180812 | |||||||||||||||||||||
45 | AFFDLTRBox003AFWALTR | 39015095307255 | 81-3091 | Vol. 1 | Numerical aircraft design using 3-D transonic analysis with optimization. Volume 1, Executive summary / | 1192562740 | ||||||||||||||||||||
46 | AFFDLTRBox003AFWALTR | 39015095307271 | 81-3091 | Vol. 2 Part 2 | Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Fighter design / | 1192562738 | ||||||||||||||||||||
47 | AFFDLTRBox003AFWALTR | 39015095307263 | 81-3091 | Vol. 2 Part 1 | Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Transport design / | 1192562739 | ||||||||||||||||||||
48 | AFFDLTRBox003AFWALTR | 39015095307289 | 81-3091 | Vol. 3 Part 1 | Numerical aircraft design using 3-D transonic analysis with optimization. Volume 3 Part 1, User's guide to transport design computer programs / | 1192562695 | ||||||||||||||||||||
49 | AFWALBox 1 | 39015095307347 | 81-3108 | Investigation of high-AOA flying qualities : criteria and design guides / | 1193578137 | |||||||||||||||||||||
50 | AFWALBox 1 | 39015095307339 | 81-3124 | Optimality criterion methods in structural optimization / | 1193578138 | |||||||||||||||||||||
51 | AFWALBox 1 | 39015095307321 | 81-3130 | Development feasibility of missile datcom / | 1193578139 | |||||||||||||||||||||
52 | AFWALBox 1 | 39015095307586 | 81-3158 | Experimental and numerical analysis of axially compressed circular cylindrical fiber-reinforced panels with various boundary conditions / | 977302828 | |||||||||||||||||||||
53 | AFWALBox 1 | 39015095307313 | 81-3173 | Hereditary models for airfoils in unsteady aerodynamics : numerical approximations and parameter estimation / | 1193578141 | |||||||||||||||||||||
54 | AFWALBox 1 | 39015095307305 | 81-3176 | Heat transfer measurements in cold wind tunnels / | 1193578142 | |||||||||||||||||||||
55 | AFWALBox 1 | 39015095307578 | 81-3179 | Development of an aeroacoustic methodology to evaluate heatshield material performance / | 429915136 | |||||||||||||||||||||
56 | AFWALBox 1 | 39015095307412 | 81-4175 | Optimal design of simple symmetric laminates under the first ply failure criteria / | 1193578144 | |||||||||||||||||||||
57 | AFWALBox 1 | 39015095307297 | 81-4183 | Instructions for TI-59 combined card/module calculations for in-plane properties of symmetric hybrid laminates / | 1193578143 | |||||||||||||||||||||
58 | AFWALBox 1 | 39015095307404 | 82-2113 | Numerical modelling of ramjet combustors / | 1193578145 | |||||||||||||||||||||
59 | AFWALBox 1 | 39015095307396 | 82-3002 | Study of the effect of free-stream turbulence upon disturbances in the pre-transitional laminar boundary layer / | 1193577979 | |||||||||||||||||||||
60 | AFWALBox 1 | 39015095307388 | 82-3007 | Vol. 1 | Multifunction flight control reference system. Volume 1, Design and development / | 1193577980 | ||||||||||||||||||||
61 | AFWALBox 1 | 39015095307370 | 82-3021 | Flight test of advanced digital control concepts / | 1193577981 | |||||||||||||||||||||
62 | AFWALBox 1 | 39015095307362 | 82-3022 | Elements of simulation error analysis / | 1193578146 | |||||||||||||||||||||
63 | AFWALBox 1 | 39015095307354 | 82-3023 | Evaluation of a damage accumulation monitoring system as an individual aircraft tracking concept / | 1193577982 | |||||||||||||||||||||
64 | AFWALBox 1 | 39015095307560 | 82-3030 | Effects of variations in coldworking repair procedures on flaw growth and structural life / | 430180336 | |||||||||||||||||||||
65 | AFWALBox002 | 39015095299023 | 82-3031 | Introduction to computational aerodynamics / | 1240441556 | |||||||||||||||||||||
66 | AFWALBox002 | 39015095299171 | 82-3057 | Improved dynamic models for air combat analysis / | 756226707 | |||||||||||||||||||||
67 | AFWALBox002 | 39015095299320 | 82-3059 | Proceedings : ejector workshop for aerospace applications / | 1240441515 | |||||||||||||||||||||
68 | AFWALBox 1 | 39015095307545 | 82-3061 | Transient heat flow along uni-directional fibers in composites / | 1193578159 | |||||||||||||||||||||
69 | AFWALBox 1 | 39015095307537 | 82-3064 | Design criteria for the future of flight controls : proceedings of the Flight Dynamics Laboratory Flying Qualities and Flight Control Symposium, 2-5 March, 1982. | 946009295 | |||||||||||||||||||||
70 | AFWALBox 1 | 39015095307529 | 82-3067 | Real-time optimal control and differential game aircraft control algorithms for one-on-one combat / | 1193578160 | |||||||||||||||||||||
71 | AFWALBox 1 | 39015095307495 | 82-3075 | Numerical simulation of flow around a three-dimensional turret / | 1193578161 | |||||||||||||||||||||
72 | AFWALBox 1 | 39015095307503 | 82-3076 | Matrix-dominated time-dependent deformation and damage of graphite epoxy composite experimental data under ramp loading / | 430180545 | |||||||||||||||||||||
73 | AFWALBox 1 | 39015095307511 | 82-3081 | Vol. 1 | Proposed MIL standard and handbook : flying qualities of air vehicles / | 946012509 | ||||||||||||||||||||
74 | AFWALBox 1 | 39015095307420 | 82-3081 | Vol. 2 | Proposed MIL standard and handbook : flying qualities of air vehicles / | 946012509 | ||||||||||||||||||||
75 | AFWALBox 1 | 39015095307438 | 82-3086 | Graphic method for predicting audibility of noise sources / | 1139354586 | |||||||||||||||||||||
76 | AFWALBox 1 | 39015095307446 | 82-3087 | Vol. 1 | Automated design of damage resistant structures / | 11012805 | ||||||||||||||||||||
77 | AFWALBox 1 | 39015095307453 | 82-3087 | Vol. 2 | Automated design of damage resistant structures / | 11012805 | ||||||||||||||||||||
78 | AFWALBox 1 | 39015095307461 | 82-3088 | Vol. 1 | Force method optimization II. Volume I, Theoretical development / | 1193578162 | ||||||||||||||||||||
79 | AFWALBox 1 | 39015095307552 | 82-3088 | Vol. 2 | Force method optimization II. Volume II, User's manual / | 1193578158 | ||||||||||||||||||||
80 | AFWALBox 1 | 39015095307479 | 82-3103 | Advanced fatigue damage development in graphite epoxy laminates / | 430195566 | |||||||||||||||||||||
81 | AFWALBox 1 | 39015095307487 | 82-3109 | Evaluation of a biaxial test fixture : interim report for period April 1981-October 1982 / | 12392730 | |||||||||||||||||||||
82 | AFWALBox 3 | 39015095307644 | 82-3112 | Mach 0.6 to 3.0 flows over rectangular cavities / | 1195928940 | |||||||||||||||||||||
83 | AFWALBox 3 | 39015095307651 | 82-4004 | Properties of organic matrix short fiber composites / | 1195927686 | |||||||||||||||||||||
84 | AFWALBox 3 | 39015095307669 | 82-4081 | Revised instructions for TI-59 combined card/module calculations for in-plane and flexural properties of symmetric laminates / | 1195927685 | |||||||||||||||||||||
85 | AFWALBox 3 | 39015095307677 | 83-3001 | Efficient ADI and spline ADI methods for the Navier-Stokes equations / | 1195928908 | |||||||||||||||||||||
86 | AFWALBox 3 | 39015095307685 | 83-3002 | Thermal conductivities and diffusivities of graphite-epoxy composites / | 1195928935 | |||||||||||||||||||||
87 | AFWALBox 3 | 39015095307693 | 83-3018 | Transient heat flow across unidirectional fibers in composites / | 861666714 | |||||||||||||||||||||
88 | AFWALBox 3 | 39015095307701 | 83-3036 | Multivariable flight control design with uncertain parameters / | 1195928934 | |||||||||||||||||||||
89 | AFWALBox004 | 39015095321439 | 83-3037 | Stability analysis of the compressible, adiabatic similar boundary layer equations (lower branch) / | 1255716751 | |||||||||||||||||||||
90 | AFWALBox004 | 39015095321447 | 83-3041 | Study of digitally controlled flight control actuation / | 1255716750 | |||||||||||||||||||||
91 | AFWALBox004 | 39015095321454 | 83-3043 | Semielliptical cracks along holes in plates and lugs / | 430233985 | |||||||||||||||||||||
92 | AFWALBox004 | 39015095321462 | 83-3044 | Asymptotic far field conditions for unsteady subsonic and transonic flows / | 976767294 | |||||||||||||||||||||
93 | AFWALBox004 | 39015095321470 | 83-3056 | Matrix-dominated time-dependent deformation and damage of graphite-epoxy composite : experimental data under multiple-step relaxation / | 78009042 | |||||||||||||||||||||
94 | AFWALBox004 | 39015095321488 | 83-3058 | Numerical solutions for steady and unsteady oscillatory flow about an axi-symmetric inlet / | 1255716749 | |||||||||||||||||||||
95 | AFWALBox004 | 39015095321496 | 83-3059 | Tentative STOL flying qualities criteria for MIL standard and handbook / | 757678749 | |||||||||||||||||||||
96 | AFWALBox004 | 39015095321504 | 83-3060 | Fatigue/impact studies in laminated composites / | 430234894 | |||||||||||||||||||||
97 | AFWALBox004 | 39015095321512 | 83-3067 | Stability of a pair of stationary vortices in the leeward side of a cylinder in a potential flowfield / | 1255716791 | |||||||||||||||||||||
98 | AFWALBox004 | 39015095321520 | 83-3080 | Horizontal shear testing of woven fiberglass/epoxy composites / | 430329567 | |||||||||||||||||||||
99 | AFWALBox004 | 39015095321538 | 83-3087 | Thrust augmentation study of high performance ejectors / | 1255716790 | |||||||||||||||||||||
100 | AFWALBox004 | 39015095321546 | 83-3098 | Proceedings of the workshop on multivariable control systems / | 33318475 |