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Posts
- Category: AERONAUTICS (continued)
- Three-Dimensional Flows and Hypersonic Vehicles
- . Direct Numerical Simulation
- Some Important NASA CFD Computer Codes
- NASA and Computational Structural Analysis
- Structural Analysis Prior to Computers
- The Advent of Direct Analog Computers
- Digital Computation Triggers Automated Structural Analysis
- NASA Spawns NASTRAN, Its Greatest Computational Success
- Origins of NASTRAN
- Early Use and Continuing Development of NASTRAN
- Moving to Diversify and Commercialize NASTRAN
- NASA Centers and Their Computational Structural Research
- Ames Research Center
- Dryden Flight Research Center
- Glenn (Formerly Lewis) Research Center
- Goddard Space Flight Center
- Jet Propulsion Laboratory
- Johnson Space Center
- Langley Research Center
- Marshall Space Flight Center
- Applying Computational Structural Analysis to Flight Research
- YF-12 Thermal Loads and Structural Dynamics
- Modern Rotor Aerodynamic Limits Survey
- AD-1 Oblique Wing Demonstrator
- Computational Methods, Industrial Transfer, and the Way Ahead
- NASTRAN Users' Colloquia, 1971-1993
- Miscellaneous NASA Structural Analysis Programs
- FLEXSTAB (Ames, Dryden, and Langley Research Centers, 1970s)
- ANSYMP Computer Program (Glenn Research Center, 1983)
- Structural Tailoring of Engine Blades (STAEBL, Glenn, 1985)
- TRansfer ANalysis Code to Interface Thermal and Structural (3D TRANCITS, Glenn, 1985)
- COmposite Blade STRuctural ANalyzer (COBSTRAN, Glenn, 1989)
- NPLOT (Goddard, 1982)
- Dynamic Simulation of Controls & Structure (Goddard, 1970s-1990s)
- Antenna Design and Analysis (JPL)
- Structural Analysis of General Shells (STAGS) (Marshall and Langley, 1960s-present)
- Structural Analysis and Loads Prediction Facilities
- Spin Rig (Glenn Research Center
- High-Temperature Structures and Materials
- The High-Speed Environment
- Metals, Ceramics, and Composites
- Ablative and Radiative Structures
- Hot Structures: Dyna-Soar
- Hot Structures: ASSET
- Reusable Surface Insulation
- Cooling
- Turbine Blades
- Blade Fabrication
- Materials Research and Development: The NASP Legacy
- Making the Electric Jet
- Aircraft Flight Control: Beginnings to the 1950s
- Fly-By-Wire: The Beginnings
- Early Aircraft Fly-By-Wire Applications
- Space Race and the War in Vietnam: Emphasis on FBW Accelerates
- The Air Force JB-47E Fly-By-Wire Project
- Project 680J: Survivable Flight Control System YF-4E
- The Precision Aircraft Control Technology YF-4E Program
- European FBW Research Efforts
- Understanding of FBW Benefits
- Digital Fly-By-Wire: The Space Legacy
- The NASA Digital Fly-By-Wire F-8 Program
- F-8 DFBW: Phase I
- DFBW F-8: Phase II
- DFBW F-8: An Appreciation
- The Lightweight Fighter Program and the YF-16
- F-16 CCV
- YC-14
- Advanced Fighter Technology Integration F-16 Program
- AFTI Phase I Testing
- Phase II Testing
- Strike Technology Testbed
- Power-By-Wire Testbed
- Technology Transfer and Lessons Learned
- NASA Observations
- Aircraft Certification Contributions
- YA-7D DIGITAC
- Highly Maneuverable Aircraft Technology
- International CCV Flight Research Efforts
- U. K. Jaguar ACT
- French Mirage NG
- Japanese CCV T-2
- X-29
- X-31 Enhanced Fighter Maneuverability Demonstrator
- Digital Electronic Engine Control
- Highly Integrated Digital Electronic Control
- Adaptive Engine Control System
- Performance Seeking Control
- Self-Repairing Flight Control System
- Propulsion Controlled Aircraft System
- NF-15B Advanced Control Technology: Air Force S/MTD
- NASA Advanced Control Technology for Integrated Vehicles
- High Stability Engine Control
- Intelligent Flight Control System
- The Continuing Legacy of FBW Research in Aircraft Development
- Advancing Propulsive Technology
- Noise Pollution Forces Engine Improvements
- Quiet Clean Short Haul Experimental Engine
- Aircraft Energy Efficiency Program
- Engine Component Improvement Project
- Energy Efficient Engine Project