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A Summary of Airframe Results from a Fokker F28 Full-Scale Crash Test
Finite Element Simulations of Two Vertical Drop Tests of F-28 Fuselage Sections
Adjoint-Based Methodology for Time-Dependent Optimal Control (AMTOC)
CFL3D Contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop
Sensitivity Analysis for Multidisciplinary Systems (SAMS)
Photogrammetry Methodology Development for Gossamer Spacecraft Structures
Wind-US Unstructured Flow Solutions for a Transonic Diffuser
Study of active vibration isolation systems for severe ground transportation environments
Advanced feed system component interaction analysis Quarterly status letter, 30 Jun. - 30 Sep. 1969
Nearfield Anisotropic Mesh Adaptation for the Third AIAA Sonic Boom Workshop
Some experiences with active control of aeroelastic response
Finite-Element Analysis of a Mach-8 Flight Test Article Using Nonlinear Contact Elements
Preliminary Results from Propellant Mass Gauging with Electrical Capacitance Tomography
Mariner Venus 67 structural developmental and qualification vibration test report
Progress in aeroelastic optimization - Analytical versus numerical approaches
A design study for the incorporation of aeroelastic capability into NASTRAN
Characteristics of Separated Flow Regions Within Altitude Compensating Nozzles Final Report
Progress of CFM Model Development and Validation at NASA Glenn Research Center
Recent Improvements to the Copernicus Trajectory Design and Optimization System
Reducing Landing Site Contamination Using 3-D Trajectory Optimization for Surface Hoppers
The Shock and Vibration Bulletin
Overdeterministic Fracture Analysis and Singular Value Decomposition
The Mariner 6 and 7 Flight Paths and Their Determination from Tracking Data
Nonlinear Unsteady Aerodynamic Modeling Using Wind Tunnel and Computational Data
Generalized Fluid System Simulation Program, Version 6.0
Dynamic Flight Maneuvering Using Virtual Control Surfaces Generated by Trapped Vorticity
ANDES TOOLS: Promotional slides for Industrial Clients
Exploring the Accuracy of RANS Simulations for Mars Entry Vehicles
Computational Aeroservoelastic Analysis with an Euler-Based Unsteady Flow Solver
Computation of design parameters and visualization of Goertler vortices
A Shock Tube Driver with a 'Cyclone' Separator
Importance of Thermostructural Testing Hypersonic Structures [STUB]