Barcode/UNT Number

Electr. OCLC No.

HT/UNT Status

Advanced residual strength degradation rate modeling for advanced composite structures. Volume 1. Task I: Preliminary screening /

Advanced residual strength degradation rate Modeling for advanced composite structures. Volume 2. Tasks II and III /

Advanced residual strength degradation rate modeling for advanced composite structures. Volume 3. Appendixes to report for Tasks II and III /

OPTIM III : a NASTRAN compatible large scale automated minimum weight design problem-users and programmers manual /

Computation of three-dimensional supersonic viscous flows in internal corners /

Response of nonlinear structural panels subjected to high intensity noise /

Sonic fatigue design techniques for advanced composite aircraft structures : Final report /

Development of a nozzle to improve the turning of supersonic Coanda jets /

Weapon bay cavity noise environments, data correlation and prediction for the B-1 aircraft /

High angle of attack missile aerodynamics at Mach numbers 0.30 to 1.5 /

Aerodynamic configured missile development final report. Volume V, Phase II experimental program /

Aerodynamic configured missile development : final report. Volume I, Executive Summary /

Volume II, Appendix A

Aerodynamic configured missile development : final report. Volume II, Appendix A, Configuration Development. Aerodynamic configured missile reference library summary /

Volume II, Appendix B

Aerodynamic configured missile development : final report. Volume II, Appendix B, Configuration Development. Relations between aerodynamic characteristics and performance /

Aerodynamic configured missile development : final report. Volume III, Missile aerodynamic prediction rationale using the Supersonic/Hypersonic arbitrary body program /

Aerodynamic configured missile development : final report. Volume IV, Phase I experimental program /

Aerodynamic configured missile development : final report. Volume VI, Phase III experimental program /

http://digital.library.unt.edu/ark:/67531/metadc1536329/

http://digital.library.unt.edu/ark:/67531/metadc1536328/

Advanced ejection seat for high dynamic pressure escape wind tunnel test report /

Finite span effects on flap heating and effectiveness in a turbulent boundary layer /

Use of strained coordinate perturbation method in transonic aeroelestic computations /

Aerodynamic analysis of a fighter aircraft with a higher order paneling method /

Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume I, Surface streamline tracing /

Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume II, Computer graphics /

Use of strained coordinate perturbation method in transonic aeroelestic computations /

Study to determine the effect of glass compositional variations on vibration damping properties /

Relationship between tensile strength and flexure strength in fiber reinforced composites /

Coaxial dump ramjet combustor combustion instabilities. Part I. Parametric test data /

Research on turbine rotor-stator aerodynamic interaction and rotor negative incidence stall /

Effects of fighter attack spectrum on composite fatigue life /

Evaluation of USSAERO and HABP computer codes for aerodynamic predictions for slender bodies /

Source-Doublet approach to modeling triple ejector rack store configurations and force calculations /

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Panel optimization with integrated software (POIS). Volume 1, Panda -- interactive program for preliminary minimum weight design /

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Panel optimization with integrated software (POIS). Volume 2, User instructions -- Echo and RRSYS /

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AFFDLTRBox003AFWALTR

Numerical aircraft design using 3-D transonic analysis with optimization. Volume 1, Executive summary /

AFFDLTRBox003AFWALTR

Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Fighter design /

AFFDLTRBox003AFWALTR

Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Transport design /

AFFDLTRBox003AFWALTR

Numerical aircraft design using 3-D transonic analysis with optimization. Volume 3 Part 1, User's guide to transport design computer programs /

Investigation of high-AOA flying qualities : criteria and design guides /

Experimental and numerical analysis of axially compressed circular cylindrical fiber-reinforced panels with various boundary conditions /

Hereditary models for airfoils in unsteady aerodynamics : numerical approximations and parameter estimation /

Development of an aeroacoustic methodology to evaluate heatshield material performance /

Optimal design of simple symmetric laminates under the first ply failure criteria /

Instructions for TI-59 combined card/module calculations for in-plane properties of symmetric hybrid laminates /

Study of the effect of free-stream turbulence upon disturbances in the pre-transitional laminar boundary layer /

Multifunction flight control reference system. Volume 1, Design and development /

Evaluation of a damage accumulation monitoring system as an individual aircraft tracking concept /

Effects of variations in coldworking repair procedures on flaw growth and structural life /

Proceedings : ejector workshop for aerospace applications /

Transient heat flow along uni-directional fibers in composites /

Design criteria for the future of flight controls : proceedings of the Flight Dynamics Laboratory Flying Qualities and Flight Control Symposium, 2-5 March, 1982.

Real-time optimal control and differential game aircraft control algorithms for one-on-one combat /

Numerical simulation of flow around a three-dimensional turret /

Matrix-dominated time-dependent deformation and damage of graphite epoxy composite experimental data under ramp loading /

Proposed MIL standard and handbook : flying qualities of air vehicles /

Proposed MIL standard and handbook : flying qualities of air vehicles /

Force method optimization II. Volume I, Theoretical development /

Advanced fatigue damage development in graphite epoxy laminates /

Evaluation of a biaxial test fixture : interim report for period April 1981-October 1982 /

Revised instructions for TI-59 combined card/module calculations for in-plane and flexural properties of symmetric laminates /

Efficient ADI and spline ADI methods for the Navier-Stokes equations /

Thermal conductivities and diffusivities of graphite-epoxy composites /

Transient heat flow across unidirectional fibers in composites /

Multivariable flight control design with uncertain parameters /

Stability analysis of the compressible, adiabatic similar boundary layer equations (lower branch) /

Asymptotic far field conditions for unsteady subsonic and transonic flows /

Matrix-dominated time-dependent deformation and damage of graphite-epoxy composite : experimental data under multiple-step relaxation /

Numerical solutions for steady and unsteady oscillatory flow about an axi-symmetric inlet /

Tentative STOL flying qualities criteria for MIL standard and handbook /

Stability of a pair of stationary vortices in the leeward side of a cylinder in a potential flowfield /

Horizontal shear testing of woven fiberglass/epoxy composites /

Proceedings of the workshop on multivariable control systems /