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Integrated Thermal Response Modeling System For Hypersonic Entry Vehicles
On-Engine Investigation of SCR on Filters (SCRoF) for HDD Passive Applications
Effect of wave-inclusion interactions in the crosshole tomographic imaging of heterogeneous media
Effect of wave-inclusion interactions in the crosshole tomographic imaging of heterogeneous media
Level-Set Topology Optimization with Aeroelastic Constraints
FPI and MPI of Cracks Under Coatings
Cart3D Simulations for the First AIAA Sonic Boom Prediction Workshop
An Approach to the Design and Implementation of Spacecraft Attitude Control Systems
Morpheus 1.5A Lander Failure Investigation Results
Thermal Performance of Disc Brake and CFD Analysis
NB-Rail - die Koordinierungsgruppe der benannten Stellen in Europa
Transitioning Active Flow Control to Applications
Sources of helicopter rotor hub inplane shears
Recent advances in integrated multidisciplinary optimization of rotorcraft
On-line analysis capabilities developed to support the AFW wind-tunnel tests
Parallel dynamic programming for on-line flight path optimization
Delta II secondary payload opportunities for tether demonstration experiments
Description of an experimental expert system flight status monitor
Spacecraft attitude control for a solar electric geosynchronous transfer mission
Emissions Certification Vehicle Cycles Based on Heavy Duty Engine Test Cycles
Neue Methodik von Belastungsversuchen an massiven Eisenbahnbrücken
Analysis of Shuttle Orbiter Reliability and Maintainability Data for Conceptual Studies
Subscale Test Program for the Orion Conical Ribbon Drogue Parachute
Singular control in minimum time spacecraft reorientation
An aircraft model for the AIAA controls design challenge
A method for optimal actuator and sensor placement for large flexible structures
Simulated rotor test apparatus dynamic characteristics in the 80- by 120-foot wind tunnel
Recent Advances in Multidisciplinary Analysis and Optimization, part 1
Approach to transaction management for Space Station Freedom
Optimal decentralized feedback control for a truss structure
Interactive systems design and synthesis of future spacecraft concepts
Automated wing structural design
Development and Testing of Automatically Generated ACS Flight Software for the MAP Spacecraft
An approach to the design and implementation of spacecraft attitude control systems
Acoustic monitoring of prestressed concrete cylinder pipe
Delta II/Geotail Pre-Launch Press Conference
Sensitivity of Space Station Alpha Joint robust controller to structural modal parameter variations
Hot-bench simulation of the active flexible wing wind-tunnel model
Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport
Nineteenth Space Simulation Conference Cost Effective Testing for the 21st Century
Structural Tailoring/Analysis for Hypersonic Components - A computational simulation