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Box
Barcode/UNT Number
SuffixTitlePrint OCLC No.
Electr. OCLC No.
Serial Info
HT/UNT Status
HT/UNT-LinksNotes
2
AFWALBox0023901509533492979-3095Volume I
Advanced residual strength degradation rate modeling for advanced composite structures. Volume 1. Task I: Preliminary screening /
429474239
3
AFWALBox0023901509533477079-3095Volume II
Advanced residual strength degradation rate Modeling for advanced composite structures. Volume 2. Tasks II and III /
429472669
4
AFWALBox0023901509533462279-3095Volume III
Advanced residual strength degradation rate modeling for advanced composite structures. Volume 3. Appendixes to report for Tasks II and III /
429484244
5
AFWALBox0023901509533463080-3007
OPTIM III : a NASTRAN compatible large scale automated minimum weight design problem-users and programmers manual /
1240441416
6
AFWALBox0023901509533464880-3017
Computation of three-dimensional supersonic viscous flows in internal corners /
1240441174
7
AFWALBox0023901509533478880-3018
Response of nonlinear structural panels subjected to high intensity noise /
429650317
8
AFWALBox0023901509533479680-3019
Sonic fatigue design techniques for advanced composite aircraft structures : Final report /
429642815
9
AFWALBox0023901509533493780-3027
Development of a nozzle to improve the turning of supersonic Coanda jets /
1240441467
10
AFWALBox0023901509533494580-3045Experimental investigation of the crack growth gage /429654085
11
AFWALBox0023901509529895980-3050
Weapon bay cavity noise environments, data correlation and prediction for the B-1 aircraft /
429654561
12
AFWALBox0023901509529896780-3061
Holographic investigation of slender body vortex wakes /
1240441468
13
AFWALBox0023901509529897580-3062Hypersonic boundary layer transition experiments /1240441469
14
AFWALBox0023901509529910680-3070
High angle of attack missile aerodynamics at Mach numbers 0.30 to 1.5 /
1240441500
15
AFWALBox 13901509530759480-3071Vol. 5
Aerodynamic configured missile development final report. Volume V, Phase II experimental program /
1194593907
16
AFWALBox0023901509529911480-3071Volume I
Aerodynamic configured missile development : final report. Volume I, Executive Summary /
1240441502
17
UNTBox115UNT80-3071Volume IIAerodynamic configured missile development : final report. Volume II, Configuration development /1245936725
http://digital.library.unt.edu/ark:/67531/metadc1536329/
18
AFWALBox0023901509529912280-3071
Volume II, Appendix A
Aerodynamic configured missile development : final report. Volume II, Appendix A, Configuration Development. Aerodynamic configured missile reference library summary /
1240441089
19
AFWALBox0023901509529925480-3071
Volume II, Appendix B
Aerodynamic configured missile development : final report. Volume II, Appendix B, Configuration Development. Relations between aerodynamic characteristics and performance /
1240441090
20
AFWALBox0023901509529926280-3071Volume III
Aerodynamic configured missile development : final report. Volume III, Missile aerodynamic prediction rationale using the Supersonic/Hypersonic arbitrary body program /
1240441503
21
AFWALBox0023901509529927080-3071Volume IV
Aerodynamic configured missile development : final report. Volume IV, Phase I experimental program /
1240441223
22
AFWALBox0023901509529913080-3071Volume VI
Aerodynamic configured missile development : final report. Volume VI, Phase III experimental program /
1240441504
23
UNTBox115UNT80-3073Structural design and wind tunnel testing of a forward swept fighter wing /1245936611
http://digital.library.unt.edu/ark:/67531/metadc1536328/
24
AFWALBox 13901509530760280-3084
Advanced ejection seat for high dynamic pressure escape wind tunnel test report /
1194593908
25
AFWALBox 13901509530761080-3090
Finite span effects on flap heating and effectiveness in a turbulent boundary layer /
1194593909
26
AFWALBox 13901509530762880-3102
Use of strained coordinate perturbation method in transonic aeroelestic computations /
1194593910
27
AFWALBox 33901509530786780-3115
Aerodynamic analysis of a fighter aircraft with a higher order paneling method /
1195928920
28
AFWALBox 33901509530787580-3117Vol. 1
Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume I, Surface streamline tracing /
1195928919
29
AFWALBox 33901509530788380-3117Vol. 2
Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume II, Computer graphics /
1195927707
30
AFWALBox 13901509530763680-3143
Use of strained coordinate perturbation method in transonic aeroelestic computations /
1194593911
31
AFWALBox0023901509529928880-4061
Study to determine the effect of glass compositional variations on vibration damping properties /
429655271
32
AFWALBox0023901509529929680-4104
Relationship between tensile strength and flexure strength in fiber reinforced composites /
60037128
33
AFWALBox0023901509529914880-4121Flexible fabrics from TaC-loaded carbon yarns /1240441042
34
AFWALBox0023901509529898381-2047Part I
Coaxial dump ramjet combustor combustion instabilities. Part I. Parametric test data /
1240441505
35
AFWALBox0023901509529899181-2114
Research on turbine rotor-stator aerodynamic interaction and rotor negative incidence stall /
1240441562
36
AFWALBox0023901509529900781-3001
Effects of fighter attack spectrum on composite fatigue life /
429905546
37
AFWALBox0023901509529901581-3002High speed smoke flow visualization /946213694
38
AFWALBox0023901509529915581-3021Vortex breakdown and instability /1240441043
39
AFWALBox0023901509529916381-3035
Evaluation of USSAERO and HABP computer codes for aerodynamic predictions for slender bodies /
1240441563
40
AFWALBox0023901509529930481-3036Cavity oscillation in cruise missile carrier aircraft /429908526
41
AFWALBox0023901509529931281-3059
Source-Doublet approach to modeling triple ejector rack store configurations and force calculations /
1240441514
42
AFFDLTRBox003AFWALTR
3901509530722281-3073Vol. 1
Panel optimization with integrated software (POIS). Volume 1, Panda -- interactive program for preliminary minimum weight design /
1192562742
43
AFFDLTRBox003AFWALTR
3901509530723081-3073Vol. 2
Panel optimization with integrated software (POIS). Volume 2, User instructions -- Echo and RRSYS /
1192562741
44
AFFDLTRBox003AFWALTR
3901509530724881-3079Handbook of force management methods /780180812
45
AFFDLTRBox003AFWALTR
3901509530725581-3091Vol. 1
Numerical aircraft design using 3-D transonic analysis with optimization. Volume 1, Executive summary /
1192562740
46
AFFDLTRBox003AFWALTR
3901509530726381-3091Vol. 2 Part 1
Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Transport design /
1192562739
47
AFFDLTRBox003AFWALTR
3901509530727181-3091Vol. 2 Part 2
Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Fighter design /
1192562738
48
AFFDLTRBox003AFWALTR
3901509530728981-3091Vol. 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 13901509530734781-3108
Investigation of high-AOA flying qualities : criteria and design guides /
1193578137
50
AFWALBox 13901509530733981-3124Optimality criterion methods in structural optimization /1193578138
51
AFWALBox 13901509530732181-3130Development feasibility of missile datcom /1193578139
52
AFWALBox 13901509530758681-3158
Experimental and numerical analysis of axially compressed circular cylindrical fiber-reinforced panels with various boundary conditions /
977302828
53
AFWALBox 13901509530731381-3173
Hereditary models for airfoils in unsteady aerodynamics : numerical approximations and parameter estimation /
1193578141
54
AFWALBox 13901509530730581-3176Heat transfer measurements in cold wind tunnels /1193578142
55
AFWALBox 13901509530757881-3179
Development of an aeroacoustic methodology to evaluate heatshield material performance /
429915136
56
AFWALBox 13901509530741281-4175
Optimal design of simple symmetric laminates under the first ply failure criteria /
1193578144
57
AFWALBox 13901509530729781-4183
Instructions for TI-59 combined card/module calculations for in-plane properties of symmetric hybrid laminates /
1193578143
58
AFWALBox 13901509530740482-2113Numerical modelling of ramjet combustors /1193578145
59
AFWALBox 13901509530739682-3002
Study of the effect of free-stream turbulence upon disturbances in the pre-transitional laminar boundary layer /
1193577979
60
AFWALBox 13901509530738882-3007Vol. 1
Multifunction flight control reference system. Volume 1, Design and development /
1193577980
61
AFWALBox 13901509530737082-3021Flight test of advanced digital control concepts /1193577981
62
AFWALBox 13901509530736282-3022Elements of simulation error analysis /1193578146
63
AFWALBox 13901509530735482-3023
Evaluation of a damage accumulation monitoring system as an individual aircraft tracking concept /
1193577982
64
AFWALBox 13901509530756082-3030
Effects of variations in coldworking repair procedures on flaw growth and structural life /
430180336
65
AFWALBox0023901509529902382-3031Introduction to computational aerodynamics /1240441556
66
AFWALBox0023901509529917182-3057Improved dynamic models for air combat analysis /756226707
67
AFWALBox0023901509529932082-3059
Proceedings : ejector workshop for aerospace applications /
1240441515
68
AFWALBox 13901509530754582-3061
Transient heat flow along uni-directional fibers in composites /
1193578159
69
AFWALBox 13901509530753782-3064
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 13901509530752982-3067
Real-time optimal control and differential game aircraft control algorithms for one-on-one combat /
1193578160
71
AFWALBox 13901509530749582-3075
Numerical simulation of flow around a three-dimensional turret /
1193578161
72
AFWALBox 13901509530750382-3076
Matrix-dominated time-dependent deformation and damage of graphite epoxy composite experimental data under ramp loading /
430180545
73
AFWALBox 13901509530751182-3081Vol. 1
Proposed MIL standard and handbook : flying qualities of air vehicles /
946012509
74
AFWALBox 13901509530742082-3081Vol. 2
Proposed MIL standard and handbook : flying qualities of air vehicles /
946012509
75
AFWALBox 13901509530743882-3086
Graphic method for predicting audibility of noise sources /
1139354586
76
AFWALBox 13901509530744682-3087Vol. 1Automated design of damage resistant structures /11012805
77
AFWALBox 13901509530745382-3087Vol. 2Automated design of damage resistant structures /11012805
78
AFWALBox 13901509530746182-3088Vol. 1
Force method optimization II. Volume I, Theoretical development /
1193578162
79
AFWALBox 13901509530755282-3088Vol. 2
Force method optimization II. Volume II, User's manual /
1193578158
80
AFWALBox 13901509530747982-3103
Advanced fatigue damage development in graphite epoxy laminates /
430195566
81
AFWALBox 13901509530748782-3109
Evaluation of a biaxial test fixture : interim report for period April 1981-October 1982 /
12392730
82
AFWALBox 33901509530764482-3112Mach 0.6 to 3.0 flows over rectangular cavities /1195928940
83
AFWALBox 33901509530765182-4004Properties of organic matrix short fiber composites /1195927686
84
AFWALBox 33901509530766982-4081
Revised instructions for TI-59 combined card/module calculations for in-plane and flexural properties of symmetric laminates /
1195927685
85
AFWALBox 33901509530767783-3001
Efficient ADI and spline ADI methods for the Navier-Stokes equations /
1195928908
86
AFWALBox 33901509530768583-3002
Thermal conductivities and diffusivities of graphite-epoxy composites /
1195928935
87
AFWALBox 33901509530769383-3018
Transient heat flow across unidirectional fibers in composites /
861666714
88
AFWALBox 33901509530770183-3036
Multivariable flight control design with uncertain parameters /
1195928934
89
AFWALBox0043901509532143983-3037
Stability analysis of the compressible, adiabatic similar boundary layer equations (lower branch) /
1255716751
90
AFWALBox0043901509532144783-3041Study of digitally controlled flight control actuation /1255716750
91
AFWALBox0043901509532145483-3043Semielliptical cracks along holes in plates and lugs /430233985
92
AFWALBox0043901509532146283-3044
Asymptotic far field conditions for unsteady subsonic and transonic flows /
976767294
93
AFWALBox0043901509532147083-3056
Matrix-dominated time-dependent deformation and damage of graphite-epoxy composite : experimental data under multiple-step relaxation /
78009042
94
AFWALBox0043901509532148883-3058
Numerical solutions for steady and unsteady oscillatory flow about an axi-symmetric inlet /
1255716749
95
AFWALBox0043901509532149683-3059
Tentative STOL flying qualities criteria for MIL standard and handbook /
757678749
96
AFWALBox0043901509532150483-3060Fatigue/impact studies in laminated composites /430234894
97
AFWALBox0043901509532151283-3067
Stability of a pair of stationary vortices in the leeward side of a cylinder in a potential flowfield /
1255716791
98
AFWALBox0043901509532152083-3080
Horizontal shear testing of woven fiberglass/epoxy composites /
430329567
99
AFWALBox0043901509532153883-3087
Thrust augmentation study of high performance ejectors /
1255716790
100
AFWALBox0043901509532154683-3098
Proceedings of the workshop on multivariable control systems /
33318475