Electr. OCLC No.

HT/UNT Status

Research and investigation on satellite attitude control. Part I.A, Part I. B, Summary. Design guide /

Research and investigation on satellite attitude control. Part II, Investigation of space vehicle attitude control techniques /

Investigation of hypersonic flow separation and control characteristics /

Experiments on the thermal performance of ribbon parachutes /

Dynamic stability of a system consisting of a stable parachute and an unstable load /

Aerodynamic deployable decelerator performance-evaluation program /

Investigation of hypersonic inlet shock-wave boundary layer interaction. Part I /

Ground simulator evaluations of coupled roll-spiral mode effects on aircraft handling qualities /

Analytical study of V/STOL handling qualities in hover and transition /

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.

Stress analysis of a fully inflated ribless guide surface parachute /

Experimental and analytical investigation of hypersonic inlet boundary layers /

Experimental and analytical investigation of hypersonic inlet boundary layers /

Experimental verification of the analyses and computer programs concerning heat transfer through semitransparent materials /

Study of conventional airplane handling qualities requirements. Part 1, Roll handling qualities /

Study of conventional airplane handling qualities requirements. Part 2, Lateral-directional oscillatory handling qualities /

Effects of design parameters and local flow fields on the performance of hyperflo supersonic parachutes and high dynamic pressure parachute concepts /

Analysis of the influences of different parameters on a reaction jet single-axis satellite attitude control system /

General instability of orthotropically stiffened cylinders. Part 1, Axial compression, torsion and hydrostatic pressure loadings /

General instability of orthotropically stiffened cylinders. Part 2, Bending and combined compression and bending /

Analysis of flexible aircraft structural mode control. Part 1, Unclassified data /

Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16 /

Statics and stability of thin-walled elastic beams. Part 1, Formulation of fundamental equations /

Statics and stability of thin-walled elastic beams. Part 2, Solution of equations /

Analytical determination of the thermal response of a typical aircraft structure subjected to transient external heating and cooling /

Matrix analysis methods for anisotropic inelastic structures /

Pressure distribution during parachute opening. Phase I, Infinite mass operating case /

Experimental study of the distribution of convective heat transfer to a large-scale model of parachute cloth /

Mathematical analysis of heat conduction in a sector of a hollow circular cylinder /

Development of experimental testing programs to verify thermal stress analysis /

Investigation of numerical techniques as applied to digital flight control systems /

Effects of manipulator restraints on human operator performance /

Development design methods for predicting hypersonic aerodynamic control characteristics /

Study of the influence of geometry on the strength of fatigue cracked panels /

Study of heavy equipment aerial delivery and retrieval techniques /

Automated method for the large deflection and instability analysis of three-dimensional truss and frame assemblies /

Calculated values of transient and steady state performance characteristics of man-carrying, cargo, and extraction parachutes /

Drag and dynamics of single and clustered parachutes in freestream, and with wake and ground effects /

Investigation of cross wind effects on stable parachute point-mass systems /

Investigation of the flow field during the inflation of clustered parachutes /

Transient analysis of heat conduction through a slab by infinite series /

Demonstration of a transonic box method for unsteady aerodynamics of planar wings /

Cyclic state of materials and the relationship to mechanical properties and fatigue /

Human pilot dynamic response in single-loop systems with compensatory and pursuit displays /

Development of procedures for large scale automated minimum weight structural design /

Optimum structural design concepts for aerospace vehicles : Bibliography and assessment /

Upper and lower bounds to structural deformations by dual analysis in finite elements /

FORMAT II - Second version of Fortran matrix abstraction technique. Volume 3, A User-coded matrix generator for the force method /

FORMAT II : Second version of Fortran matrix abstraction technique : Volume 4. A User-coded matrix generator for the displacement method /

FORMAT : Fortran matrix abstraction technique. Volume V, Supplement I. Engineering user and technical report extended /

FORMAT : Fortran matrix abstraction technique. Volume V. Engineering user and technical report /

FORMAT : Fortran matrix abstraction technique. Volume 5, Supplement II. Engineering user and technical report-extended /

FORMAT : Fortran matrix abstraction technique. Volume 6. Description of digital computer program - Phase 1 /

FORMAT : Fortran matrix abstraction technique. Volume 6 - Supplement 2. Description of digital computer program - Phase 1 - Extended /

FORMAT : Fortran matrix abstraction technique. Volume VII. Description of digital computer program - Phase 3 /

FORMAT : Fortran matrix abstraction technique. Volume 7 - Supplement 1. Description of digital computer program - Phase 3 - Extended /

Influence of residual stresses and thermal gradients on mechanism of buckling of shallow spherical shells /

Investigation of ablation effects on hypersonic dynamic stability of a 10 cone /

Analysis of several handling quality topics pertinent to advanced manned aircraft /

Digital computer program for the analysis of crack propagation in cyclic loaded structures /

Aerodynamic Deployable Decelerator Performance-Evaluation Program : Phase 2 /

Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume I, Equations and Results /

Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume II, Program details and operating procedure /

Method of characteristics for three-dimensional real-gas flows : including the digital computer program details and operating procedures for frozen flows /

Retical studies of configurations having high lift-to-drag rations in the viscous interaction regime /

Digital simulation of a Gaussian random process having an exponential autocorrelation function /

Stability of filament wound cylinders under combined loading /

Approximate multiple configuration analysis and allocation for least weight structural design /

Control effectiveness of transverse jets interacting with a high-speed free stream. Volume I. Design charts, theoretical and experimental results /

Effects of gust velocity spatial distributions on lateral-directional response of a VTOL aircraft /

Computerized data catalog and retrieval system for deployable aerodynamic decelerators /

Inhibition of flow separation at high speed. Volume 1, Supersonic turbulent boundary layers /

Initial VTOL flight control design criteria development - discussion of selected handling qualities topics : first yearly report / John Kroll, Jr.

Behavior of extraction parachutes in the wake of a powered airplane model /

On the effects of fiber orientation and nonhomogeneity on buckling and postbuckling equilibrium behavior of fiber-reinforced cylindrical shells under uniform axial compression /

Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft. Part III, Aerodynamics /

Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft.. Part IV, Aerothermodynamics /

Large deflection and stability analysis of two-dimensional truss and frame structures /

Application of the finite element method to elastic-plastic problems of plane stress /

MAGIC : n automated general purpose system for structural analysis. Volume 1, Engineer's manual /

MAGIC : an automated general purpose system for structural analysis. Volume 2, User's manual /

Compilation of computer programs in flight vehicle technology : 1964-1967 /

Flight text investigation of transonic shock-boundary layer phenomena /

Investigation of the effects of gusts on V/STOL craft in transition and hover /

In-flight investigation of the effects of higher-order control system dynamics on longitudinal handling qualities /

Inhibition of flow separation at high speed. Volume 2, Calculation of nonadiabatic laminar boundary layers /

Inhibition of flow separation at high speed. Volume 3, Experimental results for laminar boundary layers /