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BoxBarcode/UNT NumberReport No.SuffixTitle
Print OCLC No.
Electr. OCLC No.
Serial Info
HT/UNT Status
HT/UNT-LinksNotes
2
AFFDLTRBox0043901509532189264-168
Part IA, Part IB
Research and investigation on satellite attitude control. Part I.A, Part I. B, Summary. Design guide /
1256665198
3
AFFDLTRBox0043901509532190064-168Part II
Research and investigation on satellite attitude control. Part II, Investigation of space vehicle attitude control techniques /
1256665197
4
AFFDLTRBox0043901509532191864-174
Investigation of hypersonic flow separation and control characteristics /
1256660483
5
AFFDLTRBox0043901509532192664-192
Experiments on the thermal performance of ribbon parachutes /
1256665204
6
AFFDLTRBox0043901509532193464-194
Dynamic stability of a system consisting of a stable parachute and an unstable load /
1256665203
7
AFFDLTRBox0043901509532194265-027
Aerodynamic deployable decelerator performance-evaluation program /
402770840
8
AFFDLTRBox0043901509532195965-036
Investigation of hypersonic inlet shock-wave boundary layer interaction. Part I /
1256665118
9
AMRLTRBox002AFFDLTR3901509531011965-039
Ground simulator evaluations of coupled roll-spiral mode effects on aircraft handling qualities /
402770868
10
AMRLTRBox002AFFDLTR3901509531012765-049Part 3Heating in regions of interfering flow fields /1201261588
11
AMRLTRBox002AFFDLTR3901509531013565-073
Analytical study of V/STOL handling qualities in hover and transition /
403792301
12
AMRLTRBox002AFFDLTR3901509531014365-107Part 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
AMRLTRBox002AFFDLTR3901509531015065-111
Stress analysis of a fully inflated ribless guide surface parachute /
1139394328
14
AMRLTRBox002AFFDLTR3901509531016865-123Vol. 1
Experimental and analytical investigation of hypersonic inlet boundary layers /
1201261587
15
AMRLTRBox002AFFDLTR3901509531017665-123Vol. 2
Experimental and analytical investigation of hypersonic inlet boundary layers /
1201261587
16
AMRLTRBox002AFFDLTR3901509531019265-136
Experimental verification of the analyses and computer programs concerning heat transfer through semitransparent materials /
1201261585
17
AMRLTRBox002AFFDLTR3901509531020065-138Part 1
Study of conventional airplane handling qualities requirements. Part 1, Roll handling qualities /
403913403
18
AMRLTRBox002AFFDLTR3901509531021865-138Part 2
Study of conventional airplane handling qualities requirements. Part 2, Lateral-directional oscillatory handling qualities /
403873460
19
AMRLTRBox002AFFDLTR3901509531022665-150Vol. 1
Effects of design parameters and local flow fields on the performance of hyperflo supersonic parachutes and high dynamic pressure parachute concepts /
1201261584
20
AMRLTRBox002AFFDLTR3901509531018465-153
Analysis of the influences of different parameters on a reaction jet single-axis satellite attitude control system /
1201261586
21
AMRLTRBox002AFFDLTR3901509531023465-161Part 1
General instability of orthotropically stiffened cylinders. Part 1, Axial compression, torsion and hydrostatic pressure loadings /
403873601
22
AMRLTRBox002AFFDLTR3901509531024265-161Part 2
General instability of orthotropically stiffened cylinders. Part 2, Bending and combined compression and bending /
403953574
23
AMRLTRBox002AFFDLTR3901509531025965-190Part 1
Analysis of flexible aircraft structural mode control. Part 1, Unclassified data /
37952075
24
AMRLTRBox002AFFDLTR3901509531026765-199
Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16 /
63563622
25
AMRLTRBox002AFFDLTR3901509531027565-213Part 1
Statics and stability of thin-walled elastic beams. Part 1, Formulation of fundamental equations /
405617637
26
AMRLTRBox002AFFDLTR3901509531028365-213Part 2
Statics and stability of thin-walled elastic beams. Part 2, Solution of equations /
405631101
27
AMRLTRBox002AFFDLTR3901509531029165-218Estimation of flying qualities of piloted airplanes /989065133
28
AMRLTRBox002AFFDLTR3901509531030965-219
Analytical determination of the thermal response of a typical aircraft structure subjected to transient external heating and cooling /
405624388
29
AMRLTRBox002AFFDLTR3901509531031765-220
Matrix analysis methods for anisotropic inelastic structures /
405617853
30
AMRLTRBox002AFFDLTR3901509531032566-003
Re-entry vehicle control system design and mechanization /
1201261583
31
AMRLTRBox002AFFDLTR3901509531033366-010Phase 1
Pressure distribution during parachute opening. Phase I, Infinite mass operating case /
55756434
32
AMRLTRBox002AFFDLTR3901509531034166-013
Experimental study of the distribution of convective heat transfer to a large-scale model of parachute cloth /
405639280
33
AMRLTRBox002AFFDLTR3901509531035866-016
Mathematical analysis of heat conduction in a sector of a hollow circular cylinder /
405684983
34
AMRLTRBox002AFFDLTR3901509531036666-067
Development of experimental testing programs to verify thermal stress analysis /
406353002
35
AMRLTRBox002AFFDLTR3901509531037466-068
Investigation of numerical techniques as applied to digital flight control systems /
406359255
36
AFFDLTRBox0023901509531038266-072
Effects of manipulator restraints on human operator performance /
406379501
37
AFFDLTRBox0023901509531039066-073
Aerodynamic characteristics of non-straight-taper wings /
21434957
38
AFFDLTRBox0023901509531040866-085
Development design methods for predicting hypersonic aerodynamic control characteristics /
406359463
39
AFFDLTRBox0023901509531041666-092
Study of the influence of geometry on the strength of fatigue cracked panels /
406353347
40
AFFDLTRBox0023901509531042466-097
Study of heavy equipment aerial delivery and retrieval techniques /
68622199
41
AFFDLTRBox0023901509531043266-102
Automated method for the large deflection and instability analysis of three-dimensional truss and frame assemblies /
406415918
42
AFFDLTRBox0023901509531044066-103
Calculated values of transient and steady state performance characteristics of man-carrying, cargo, and extraction parachutes /
406416018
43
AFFDLTRBox0023901509531045766-104
Drag and dynamics of single and clustered parachutes in freestream, and with wake and ground effects /
406416107
44
AFFDLTRBox0023901509531046566-105
Investigation of cross wind effects on stable parachute point-mass systems /
406416147
45
AFFDLTRBox0023901509531047366-106Vol. 1
Investigation of the flow field during the inflation of clustered parachutes /
1139352383
46
AFFDLTRBox0023901509531048166-109
Transient analysis of heat conduction through a slab by infinite series /
406422892
47
AFFDLTRBox0023901509531052366-121
Demonstration of a transonic box method for unsteady aerodynamics of planar wings /
1202253920
48
AFFDLTRBox0023901509531051566-125
Cyclic state of materials and the relationship to mechanical properties and fatigue /
1202253919
49
AFFDLTRBox0023901509531050766-137
Human pilot dynamic response in single-loop systems with compensatory and pursuit displays /
406416271
50
AFFDLTRBox0023901509531049966-138Human pilot dynamics with various manipulators /406459526
51
AFFDLTRBox0023901509531053166-150
Compilation of data on crew emergency escape systems /
1202253921
52
AFFDLTRBox0023901509531054966-180
Development of procedures for large scale automated minimum weight structural design /
406528511
53
AFFDLTRBox 0103901509532904466-188
Optimum structural design concepts for aerospace vehicles : Bibliography and assessment /
406591470
54
AFFDLTRBox 0103901509532875666-199
Upper and lower bounds to structural deformations by dual analysis in finite elements /
406614565
55
AFFDLTRBox 0103901509532890566-207Volume III
FORMAT II - Second version of Fortran matrix abstraction technique. Volume 3, A User-coded matrix generator for the force method /
407103200
56
AFFDLTRBox 0103901509532905166-210
Influence of residual stresses and thermal gradients on mechanism of buckling of shallow spherical shells /
407285855
57
AFFDLTRBox 0103901509532876466-216Translation of flexible plates and shells /407170654
58
AFFDLTRBox 0103901509532891366-230
Investigation of ablation effects on hypersonic dynamic stability of a 10 cone /
407183177
59
AFFDLTRBox 0103901509532906967-002
Analysis of several handling quality topics pertinent to advanced manned aircraft /
407170778
60
AFFDLTRBox 0103901509532877267-005
Digital computer program for the analysis of crack propagation in cyclic loaded structures /
407835877
61
AFFDLTRBox 0103901509532892167-025
Aerodynamic Deployable Decelerator Performance-Evaluation Program : Phase 2 /
407836050
62
AFFDLTRBox 0103901509532907767-040Volume I
Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume I, Equations and Results /
1196862748
63
AFFDLTRBox 0103901509532878067-040Volume III
Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume II, Program details and operating procedure /
1196862749
64
AFFDLTRBox 0103901509532893967-047
Method of characteristics for three-dimensional real-gas flows : including the digital computer program details and operating procedures for frozen flows /
63562701
65
AFFDLTRBox 0103901509532879867-050
Retical studies of configurations having high lift-to-drag rations in the viscous interaction regime /
1196862750
66
AFFDLTRBox 0103901509532894767-052
Digital simulation of a Gaussian random process having an exponential autocorrelation function /
408550889
67
AFFDLTRBox 0103901509532908567-055
Stability of filament wound cylinders under combined loading /
408615946
68
AFFDLTRBox 0103901509532909367-059
Approximate multiple configuration analysis and allocation for least weight structural design /
408550974
69
AFFDLTRBox 0103901509529850467-089Parametric fatigue analysis of USAF aircraft /45954564
70
AFFDLTRBox 0103901509529853867-090Volume I
Control effectiveness of transverse jets interacting with a high-speed free stream. Volume I. Design charts, theoretical and experimental results /
1196862751
71
AFFDLTRBox 0103901509529851267-093
Effects of gust velocity spatial distributions on lateral-directional response of a VTOL aircraft /
41041915
72
AFFDLTRBox 0103901509529852067-115
Computerized data catalog and retrieval system for deployable aerodynamic decelerators /
55756397
73
AFFDLTRBox 0103901509529884367-119Volume I
Inhibition of flow separation at high speed. Volume 1, Supersonic turbulent boundary layers /
416480833
74
AFFDLTRBox 0103901509529854667-150
New approaches to human-pilot/vehicle dynamic analysis /
413915041
75
AFFDLTRBox 0103901509529855367-151
Initial VTOL flight control design criteria development - discussion of selected handling qualities topics : first yearly report / John Kroll, Jr.
989065259
76
AFFDLTRBox 0103901509529856167-184Analytical design methods for aircraft structural joints /414101398
77
AFFDLTRBox 0103901509529857967-185Finite deflection, discrete element analysis of shells /414543554
78
AFFDLTRBox 0103901509529865267-197
Matrix analysis of shells : small and large displacements /
415190304
79
AFFDLTRBox 0103901509529866068-015
Behavior of extraction parachutes in the wake of a powered airplane model /
1139353052
80
AFFDLTRBox 0103901509529867868-019
On the effects of fiber orientation and nonhomogeneity on buckling and postbuckling equilibrium behavior of fiber-reinforced cylindrical shells under uniform axial compression /
415157815
81
AFFDLTRBox 0103901509529868668-024Part III
Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft. Part III, Aerodynamics /
1196862752
82
AFFDLTRBox 0103901509529869468-024Part IV
Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft.. Part IV, Aerothermodynamics /
1196862753
83
AFFDLTRBox 0103901509529870268-038
Large deflection and stability analysis of two-dimensional truss and frame structures /
415157849
84
AFFDLTRBox 0103901509529871068-039
Application of the finite element method to elastic-plastic problems of plane stress /
415396160
85
AFFDLTRBox 0103901509529872868-056Volume I
MAGIC : n automated general purpose system for structural analysis. Volume 1, Engineer's manual /
416449233
86
AFFDLTRBox 0103901509529880168-056Volume II
MAGIC : an automated general purpose system for structural analysis. Volume 2, User's manual /
416449266
87
AFFDLTRBox 0103901509529881968-066
Compilation of computer programs in flight vehicle technology : 1964-1967 /
48431194
88
AFFDLTRBox 0103901509529882768-084Volume I
Flight text investigation of transonic shock-boundary layer phenomena /
1196862627
89
AFFDLTRBox 0103901509529883568-085
Investigation of the effects of gusts on V/STOL craft in transition and hover /
416480657
90
AFFDLTRBox 0103901509529885068-119Volume II
Inhibition of flow separation at high speed. Volume 2, Calculation of nonadiabatic laminar boundary layers /
416522828
91
AFFDLTRBox 0103901509529886868-119Volume III
Inhibition of flow separation at high speed. Volume 3, Experimental results for laminar boundary layers /
416525593
92
AFFDLTRBox 0103901509529887668-119Volume IV
Inhibition of flow separation at high speed. Volume IV, Calculation of nonadiabatic laminar boundary layers on conical compression surfaces /
1196869803
93
AFFDLTRBox 0103901509529858768-149
Critical evaluation of transition from laminar to turbulent shear layers with emphasis on hypersonically traveling bodies /
35370646
94
AFFDLTRBox 0103901509529873668-159
Investigation of an integrated aircrew escape/rescue capability /
22334266
95
AFFDLTRBox 0103901509529888468-167
Correlation of aerodynamic stability and control derivatives obtained from flight tests and wind tunnel tests on the XC-142A airplane /
1196869804
96
AFFDLTRBox 0103901509532889768-180Supplement I
Development of procedures for large scale automated minimum weight structural design /
406564232
97
AFCRLBox027AFFDLTR3901509530699269-021Investigation of subsonic duct distortion /1190929932
98
AFCRLBox027AFFDLTR3901509530700869-041
Flight investigation of lateral-directional handling qualities for V/STOL aircraft in low speed maneuvering flight /
47862464
99
AFFDLTRBox0033901509530701669-059
Subsonic flutter characteristics of a variable sweep wing and horizontal tail combination /
48999794
100
AFFDLTRBox0033901509530703269-063Vol. I
Low Altitude Atmospheric Turbulence LO-LOCAT phase III interim report. Volume I, Data acquisition and analysis /
1192318870