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1 | Box | Barcode/UNT Number | Report No. | Suffix | Title | Print OCLC No. | Electr. OCLC No. | Serial Info | HT/UNT Status | HT/UNT-Links | Notes | |||||||||||||||
2 | AFFDLTRBox004 | 39015095321892 | 64-168 | Part IA, Part IB | Research and investigation on satellite attitude control. Part I.A, Part I. B, Summary. Design guide / | 1256665198 | ||||||||||||||||||||
3 | AFFDLTRBox004 | 39015095321900 | 64-168 | Part II | Research and investigation on satellite attitude control. Part II, Investigation of space vehicle attitude control techniques / | 1256665197 | ||||||||||||||||||||
4 | AFFDLTRBox004 | 39015095321918 | 64-174 | Investigation of hypersonic flow separation and control characteristics / | 1256660483 | |||||||||||||||||||||
5 | AFFDLTRBox004 | 39015095321926 | 64-192 | Experiments on the thermal performance of ribbon parachutes / | 1256665204 | |||||||||||||||||||||
6 | AFFDLTRBox004 | 39015095321934 | 64-194 | Dynamic stability of a system consisting of a stable parachute and an unstable load / | 1256665203 | |||||||||||||||||||||
7 | AFFDLTRBox004 | 39015095321942 | 65-027 | Aerodynamic deployable decelerator performance-evaluation program / | 402770840 | |||||||||||||||||||||
8 | AFFDLTRBox004 | 39015095321959 | 65-036 | Investigation of hypersonic inlet shock-wave boundary layer interaction. Part I / | 1256665118 | |||||||||||||||||||||
9 | AMRLTRBox002AFFDLTR | 39015095310119 | 65-039 | Ground simulator evaluations of coupled roll-spiral mode effects on aircraft handling qualities / | 402770868 | |||||||||||||||||||||
10 | AMRLTRBox002AFFDLTR | 39015095310127 | 65-049 | Part 3 | Heating in regions of interfering flow fields / | 1201261588 | ||||||||||||||||||||
11 | AMRLTRBox002AFFDLTR | 39015095310135 | 65-073 | Analytical study of V/STOL handling qualities in hover and transition / | 403792301 | |||||||||||||||||||||
12 | AMRLTRBox002AFFDLTR | 39015095310143 | 65-107 | Part 2 | Calculation of laminar separation with free interaction by the method of integral relations. Pt. II, Two-dimensional supersonic nonadiabatic flow and axisymmetric supersonic adiabatic and nonadiabatic flows / Jack N. Nielsen, Larry L. Lynes, Frederick K. | 987265559 | ||||||||||||||||||||
13 | AMRLTRBox002AFFDLTR | 39015095310150 | 65-111 | Stress analysis of a fully inflated ribless guide surface parachute / | 1139394328 | |||||||||||||||||||||
14 | AMRLTRBox002AFFDLTR | 39015095310168 | 65-123 | Vol. 1 | Experimental and analytical investigation of hypersonic inlet boundary layers / | 1201261587 | ||||||||||||||||||||
15 | AMRLTRBox002AFFDLTR | 39015095310176 | 65-123 | Vol. 2 | Experimental and analytical investigation of hypersonic inlet boundary layers / | 1201261587 | ||||||||||||||||||||
16 | AMRLTRBox002AFFDLTR | 39015095310192 | 65-136 | Experimental verification of the analyses and computer programs concerning heat transfer through semitransparent materials / | 1201261585 | |||||||||||||||||||||
17 | AMRLTRBox002AFFDLTR | 39015095310200 | 65-138 | Part 1 | Study of conventional airplane handling qualities requirements. Part 1, Roll handling qualities / | 403913403 | ||||||||||||||||||||
18 | AMRLTRBox002AFFDLTR | 39015095310218 | 65-138 | Part 2 | Study of conventional airplane handling qualities requirements. Part 2, Lateral-directional oscillatory handling qualities / | 403873460 | ||||||||||||||||||||
19 | AMRLTRBox002AFFDLTR | 39015095310226 | 65-150 | Vol. 1 | Effects of design parameters and local flow fields on the performance of hyperflo supersonic parachutes and high dynamic pressure parachute concepts / | 1201261584 | ||||||||||||||||||||
20 | AMRLTRBox002AFFDLTR | 39015095310184 | 65-153 | Analysis of the influences of different parameters on a reaction jet single-axis satellite attitude control system / | 1201261586 | |||||||||||||||||||||
21 | AMRLTRBox002AFFDLTR | 39015095310234 | 65-161 | Part 1 | General instability of orthotropically stiffened cylinders. Part 1, Axial compression, torsion and hydrostatic pressure loadings / | 403873601 | ||||||||||||||||||||
22 | AMRLTRBox002AFFDLTR | 39015095310242 | 65-161 | Part 2 | General instability of orthotropically stiffened cylinders. Part 2, Bending and combined compression and bending / | 403953574 | ||||||||||||||||||||
23 | AMRLTRBox002AFFDLTR | 39015095310259 | 65-190 | Part 1 | Analysis of flexible aircraft structural mode control. Part 1, Unclassified data / | 37952075 | ||||||||||||||||||||
24 | AMRLTRBox002AFFDLTR | 39015095310267 | 65-199 | Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16 / | 63563622 | |||||||||||||||||||||
25 | AMRLTRBox002AFFDLTR | 39015095310275 | 65-213 | Part 1 | Statics and stability of thin-walled elastic beams. Part 1, Formulation of fundamental equations / | 405617637 | ||||||||||||||||||||
26 | AMRLTRBox002AFFDLTR | 39015095310283 | 65-213 | Part 2 | Statics and stability of thin-walled elastic beams. Part 2, Solution of equations / | 405631101 | ||||||||||||||||||||
27 | AMRLTRBox002AFFDLTR | 39015095310291 | 65-218 | Estimation of flying qualities of piloted airplanes / | 989065133 | |||||||||||||||||||||
28 | AMRLTRBox002AFFDLTR | 39015095310309 | 65-219 | Analytical determination of the thermal response of a typical aircraft structure subjected to transient external heating and cooling / | 405624388 | |||||||||||||||||||||
29 | AMRLTRBox002AFFDLTR | 39015095310317 | 65-220 | Matrix analysis methods for anisotropic inelastic structures / | 405617853 | |||||||||||||||||||||
30 | AMRLTRBox002AFFDLTR | 39015095310325 | 66-003 | Re-entry vehicle control system design and mechanization / | 1201261583 | |||||||||||||||||||||
31 | AMRLTRBox002AFFDLTR | 39015095310333 | 66-010 | Phase 1 | Pressure distribution during parachute opening. Phase I, Infinite mass operating case / | 55756434 | ||||||||||||||||||||
32 | AMRLTRBox002AFFDLTR | 39015095310341 | 66-013 | Experimental study of the distribution of convective heat transfer to a large-scale model of parachute cloth / | 405639280 | |||||||||||||||||||||
33 | AMRLTRBox002AFFDLTR | 39015095310358 | 66-016 | Mathematical analysis of heat conduction in a sector of a hollow circular cylinder / | 405684983 | |||||||||||||||||||||
34 | AMRLTRBox002AFFDLTR | 39015095310366 | 66-067 | Development of experimental testing programs to verify thermal stress analysis / | 406353002 | |||||||||||||||||||||
35 | AMRLTRBox002AFFDLTR | 39015095310374 | 66-068 | Investigation of numerical techniques as applied to digital flight control systems / | 406359255 | |||||||||||||||||||||
36 | AFFDLTRBox002 | 39015095310382 | 66-072 | Effects of manipulator restraints on human operator performance / | 406379501 | |||||||||||||||||||||
37 | AFFDLTRBox002 | 39015095310390 | 66-073 | Aerodynamic characteristics of non-straight-taper wings / | 21434957 | |||||||||||||||||||||
38 | AFFDLTRBox002 | 39015095310408 | 66-085 | Development design methods for predicting hypersonic aerodynamic control characteristics / | 406359463 | |||||||||||||||||||||
39 | AFFDLTRBox002 | 39015095310416 | 66-092 | Study of the influence of geometry on the strength of fatigue cracked panels / | 406353347 | |||||||||||||||||||||
40 | AFFDLTRBox002 | 39015095310424 | 66-097 | Study of heavy equipment aerial delivery and retrieval techniques / | 68622199 | |||||||||||||||||||||
41 | AFFDLTRBox002 | 39015095310432 | 66-102 | Automated method for the large deflection and instability analysis of three-dimensional truss and frame assemblies / | 406415918 | |||||||||||||||||||||
42 | AFFDLTRBox002 | 39015095310440 | 66-103 | Calculated values of transient and steady state performance characteristics of man-carrying, cargo, and extraction parachutes / | 406416018 | |||||||||||||||||||||
43 | AFFDLTRBox002 | 39015095310457 | 66-104 | Drag and dynamics of single and clustered parachutes in freestream, and with wake and ground effects / | 406416107 | |||||||||||||||||||||
44 | AFFDLTRBox002 | 39015095310465 | 66-105 | Investigation of cross wind effects on stable parachute point-mass systems / | 406416147 | |||||||||||||||||||||
45 | AFFDLTRBox002 | 39015095310473 | 66-106 | Vol. 1 | Investigation of the flow field during the inflation of clustered parachutes / | 1139352383 | ||||||||||||||||||||
46 | AFFDLTRBox002 | 39015095310481 | 66-109 | Transient analysis of heat conduction through a slab by infinite series / | 406422892 | |||||||||||||||||||||
47 | AFFDLTRBox002 | 39015095310523 | 66-121 | Demonstration of a transonic box method for unsteady aerodynamics of planar wings / | 1202253920 | |||||||||||||||||||||
48 | AFFDLTRBox002 | 39015095310515 | 66-125 | Cyclic state of materials and the relationship to mechanical properties and fatigue / | 1202253919 | |||||||||||||||||||||
49 | AFFDLTRBox002 | 39015095310507 | 66-137 | Human pilot dynamic response in single-loop systems with compensatory and pursuit displays / | 406416271 | |||||||||||||||||||||
50 | AFFDLTRBox002 | 39015095310499 | 66-138 | Human pilot dynamics with various manipulators / | 406459526 | |||||||||||||||||||||
51 | AFFDLTRBox002 | 39015095310531 | 66-150 | Compilation of data on crew emergency escape systems / | 1202253921 | |||||||||||||||||||||
52 | AFFDLTRBox002 | 39015095310549 | 66-180 | Development of procedures for large scale automated minimum weight structural design / | 406528511 | |||||||||||||||||||||
53 | AFFDLTRBox 010 | 39015095329044 | 66-188 | Optimum structural design concepts for aerospace vehicles : Bibliography and assessment / | 406591470 | |||||||||||||||||||||
54 | AFFDLTRBox 010 | 39015095328756 | 66-199 | Upper and lower bounds to structural deformations by dual analysis in finite elements / | 406614565 | |||||||||||||||||||||
55 | AFFDLTRBox 010 | 39015095328905 | 66-207 | Volume III | FORMAT II - Second version of Fortran matrix abstraction technique. Volume 3, A User-coded matrix generator for the force method / | 407103200 | ||||||||||||||||||||
56 | AirForceBox051AFFDL-TR | 39015104956837 | 66-207 | FORMAT II : Second version of Fortran matrix abstraction technique : Volume 4. A User-coded matrix generator for the displacement method / | 407103218 | Volume IV | ||||||||||||||||||||
57 | AirForceBox051AFFDL-TR | 39015104956795 | 66-207 | Supplement I | FORMAT : Fortran matrix abstraction technique. Volume V, Supplement I. Engineering user and technical report extended / | 406607936 | Volume V | |||||||||||||||||||
58 | AirForceBox051AFFDL-TR | 39015104956829 | 66-207 | FORMAT : Fortran matrix abstraction technique. Volume V. Engineering user and technical report / | 407068015 | Volume V | ||||||||||||||||||||
59 | AirForceBox051AFFDL-TR | 39015104956761 | 66-207 | Supplement II | FORMAT : Fortran matrix abstraction technique. Volume 5, Supplement II. Engineering user and technical report-extended / | 407110597 | Volume V | |||||||||||||||||||
60 | AirForceBox051AFFDL-TR | 39015104956738 | 66-207 | FORMAT : Fortran matrix abstraction technique. Volume 6. Description of digital computer program - Phase 1 / | 407125960 | Volume VI | ||||||||||||||||||||
61 | AirForceBox051AFFDL-TR | 39015104956811 | 66-207 | Supplement II | FORMAT : Fortran matrix abstraction technique. Volume 6 - Supplement 2. Description of digital computer program - Phase 1 - Extended / | 407149656 | Volume VI | |||||||||||||||||||
62 | AirForceBox051AFFDL-TR | 39015104956787 | 66-207 | FORMAT : Fortran matrix abstraction technique. Volume VII. Description of digital computer program - Phase 3 / | 407110845 | Volume VII | ||||||||||||||||||||
63 | AirForceBox051AFFDL-TR | 39015104956753 | 66-207 | Supplement I | FORMAT : Fortran matrix abstraction technique. Volume 7 - Supplement 1. Description of digital computer program - Phase 3 - Extended / | 407170401 | Volume VII | |||||||||||||||||||
64 | AFFDLTRBox 010 | 39015095329051 | 66-210 | Influence of residual stresses and thermal gradients on mechanism of buckling of shallow spherical shells / | 407285855 | |||||||||||||||||||||
65 | AFFDLTRBox 010 | 39015095328764 | 66-216 | Translation of flexible plates and shells / | 407170654 | |||||||||||||||||||||
66 | AFFDLTRBox 010 | 39015095328913 | 66-230 | Investigation of ablation effects on hypersonic dynamic stability of a 10 cone / | 407183177 | |||||||||||||||||||||
67 | AFFDLTRBox 010 | 39015095329069 | 67-002 | Analysis of several handling quality topics pertinent to advanced manned aircraft / | 407170778 | |||||||||||||||||||||
68 | AFFDLTRBox 010 | 39015095328772 | 67-005 | Digital computer program for the analysis of crack propagation in cyclic loaded structures / | 407835877 | |||||||||||||||||||||
69 | AFFDLTRBox 010 | 39015095328921 | 67-025 | Aerodynamic Deployable Decelerator Performance-Evaluation Program : Phase 2 / | 407836050 | |||||||||||||||||||||
70 | AFFDLTRBox 010 | 39015095329077 | 67-040 | Volume I | Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume I, Equations and Results / | 1196862748 | ||||||||||||||||||||
71 | AFFDLTRBox 010 | 39015095328780 | 67-040 | Volume III | Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume II, Program details and operating procedure / | 1196862749 | ||||||||||||||||||||
72 | AFFDLTRBox 010 | 39015095328939 | 67-047 | Method of characteristics for three-dimensional real-gas flows : including the digital computer program details and operating procedures for frozen flows / | 63562701 | |||||||||||||||||||||
73 | AFFDLTRBox 010 | 39015095328798 | 67-050 | Retical studies of configurations having high lift-to-drag rations in the viscous interaction regime / | 1196862750 | |||||||||||||||||||||
74 | AFFDLTRBox 010 | 39015095328947 | 67-052 | Digital simulation of a Gaussian random process having an exponential autocorrelation function / | 408550889 | |||||||||||||||||||||
75 | AFFDLTRBox 010 | 39015095329085 | 67-055 | Stability of filament wound cylinders under combined loading / | 408615946 | |||||||||||||||||||||
76 | AFFDLTRBox 010 | 39015095329093 | 67-059 | Approximate multiple configuration analysis and allocation for least weight structural design / | 408550974 | |||||||||||||||||||||
77 | AFFDLTRBox 010 | 39015095298504 | 67-089 | Parametric fatigue analysis of USAF aircraft / | 45954564 | |||||||||||||||||||||
78 | AFFDLTRBox 010 | 39015095298538 | 67-090 | Volume I | Control effectiveness of transverse jets interacting with a high-speed free stream. Volume I. Design charts, theoretical and experimental results / | 1196862751 | ||||||||||||||||||||
79 | AFFDLTRBox 010 | 39015095298512 | 67-093 | Effects of gust velocity spatial distributions on lateral-directional response of a VTOL aircraft / | 41041915 | |||||||||||||||||||||
80 | AFFDLTRBox 010 | 39015095298520 | 67-115 | Computerized data catalog and retrieval system for deployable aerodynamic decelerators / | 55756397 | |||||||||||||||||||||
81 | AFFDLTRBox 010 | 39015095298843 | 67-119 | Volume I | Inhibition of flow separation at high speed. Volume 1, Supersonic turbulent boundary layers / | 416480833 | ||||||||||||||||||||
82 | AFFDLTRBox 010 | 39015095298546 | 67-150 | New approaches to human-pilot/vehicle dynamic analysis / | 413915041 | |||||||||||||||||||||
83 | AFFDLTRBox 010 | 39015095298553 | 67-151 | Initial VTOL flight control design criteria development - discussion of selected handling qualities topics : first yearly report / John Kroll, Jr. | 989065259 | |||||||||||||||||||||
84 | AFFDLTRBox 010 | 39015095298561 | 67-184 | Analytical design methods for aircraft structural joints / | 414101398 | |||||||||||||||||||||
85 | AFFDLTRBox 010 | 39015095298579 | 67-185 | Finite deflection, discrete element analysis of shells / | 414543554 | |||||||||||||||||||||
86 | AFFDLTRBox 010 | 39015095298652 | 67-197 | Matrix analysis of shells : small and large displacements / | 415190304 | |||||||||||||||||||||
87 | AFFDLTRBox 010 | 39015095298660 | 68-015 | Behavior of extraction parachutes in the wake of a powered airplane model / | 1139353052 | |||||||||||||||||||||
88 | AFFDLTRBox 010 | 39015095298678 | 68-019 | On the effects of fiber orientation and nonhomogeneity on buckling and postbuckling equilibrium behavior of fiber-reinforced cylindrical shells under uniform axial compression / | 415157815 | |||||||||||||||||||||
89 | AFFDLTRBox 010 | 39015095298686 | 68-024 | Part III | Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft. Part III, Aerodynamics / | 1196862752 | ||||||||||||||||||||
90 | AFFDLTRBox 010 | 39015095298694 | 68-024 | Part IV | Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft.. Part IV, Aerothermodynamics / | 1196862753 | ||||||||||||||||||||
91 | AFFDLTRBox 010 | 39015095298702 | 68-038 | Large deflection and stability analysis of two-dimensional truss and frame structures / | 415157849 | |||||||||||||||||||||
92 | AFFDLTRBox 010 | 39015095298710 | 68-039 | Application of the finite element method to elastic-plastic problems of plane stress / | 415396160 | |||||||||||||||||||||
93 | AFFDLTRBox 010 | 39015095298728 | 68-056 | Volume I | MAGIC : n automated general purpose system for structural analysis. Volume 1, Engineer's manual / | 416449233 | ||||||||||||||||||||
94 | AFFDLTRBox 010 | 39015095298801 | 68-056 | Volume II | MAGIC : an automated general purpose system for structural analysis. Volume 2, User's manual / | 416449266 | ||||||||||||||||||||
95 | AFFDLTRBox 010 | 39015095298819 | 68-066 | Compilation of computer programs in flight vehicle technology : 1964-1967 / | 48431194 | |||||||||||||||||||||
96 | AFFDLTRBox 010 | 39015095298827 | 68-084 | Volume I | Flight text investigation of transonic shock-boundary layer phenomena / | 1196862627 | ||||||||||||||||||||
97 | AFFDLTRBox 010 | 39015095298835 | 68-085 | Investigation of the effects of gusts on V/STOL craft in transition and hover / | 416480657 | |||||||||||||||||||||
98 | AirForceBox051AFFDL-TR | 39015104956720 | 68-090 | In-flight investigation of the effects of higher-order control system dynamics on longitudinal handling qualities / | 1302642420 | |||||||||||||||||||||
99 | AFFDLTRBox 010 | 39015095298850 | 68-119 | Volume II | Inhibition of flow separation at high speed. Volume 2, Calculation of nonadiabatic laminar boundary layers / | 416522828 | ||||||||||||||||||||
100 | AFFDLTRBox 010 | 39015095298868 | 68-119 | Volume III | Inhibition of flow separation at high speed. Volume 3, Experimental results for laminar boundary layers / | 416525593 |