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Posts
- Category: A VERTICAL EMPIRE (continued)
- BK23
- BK25
- Crusade and the 54-inch Black Knight
- How Successful was Black Knight?
- Was Black Knight Good Value for Money?
- Black Arrow
- The Flights
- R1 - 4 March 1970
- R3 - 28 October 1971
- The Cancellation
- Black Arrow Improvements
- The ‘Might Have Beens’
- A Black Knight IRBM
- Could Britain Have Launched an Astronaut into Orbit?
- Alternative Histories
- Conclusions
- MINISTER OF DEFENCE
- Could the UK Once Again Become Involved in a Launcher Programme?
- Original Documents
- K11 Underground Launcher
- Use of Spadeadam for Space Firings
- Space and the Future Of The European Launcher Development Organisation (ELDO)
- A Black Knight Launcher?
- Category: AERONAUTICS
- Swing Wing: The Path to Variable Geometry
- The Quest for Refinement
- Richard Whitcomb and the Quest for Aerodynamic Efficiency
- The Making of an Engineer
- Dick Whitcomb and the Transonic-Supersonic Breakthrough
- The Path to Area Rule
- Validation in Flight
- Inventing the Supercritical Wing
- SCW Takes to the Air
- Winglets—Yet Another Whitcomb Innovation
- Whitcomb and History
- NACA-NASA and the Rotary Wing Revolution
- The Research Culture
- NACA 1930-1958: Establishing Fundamentals
- NASA 1958-1970: A Time of Transition
- NASA 1970-1990: Joint Program Momentum Peaks
- NASA 1990-2007: Coping with Institutional and Resource Challenges
- Softening the Sonic Boom: 50 Years of NASA Research
- From Curiosity to Controversy
- A Painful Lesson: Sonic Booms and the Supersonic Transport
- From SCAT Research to SST Development
- Supersonic Flight Tests and Surveys
- Laboratory Experiments and Sonic Boom Theory
- SST Reincarnated: Birth of the High-Speed Civil Transport
- Trying Once More: The High-Speed Research Program
- Proof at Last: The Shaped Sonic Boom Demonstration
- Breaking Up Shock Waves with "Quiet Spike"
- Focusing on Fundamentals: The Supersonics Project
- Perspectives on the Past, Prospects for the Future
- Toward Transatmospheric Flight: From V-2 to the X-51
- Moving Beyond the V-2: John Becker Births American Hypersonics
- Emergent Hypersonic Technology and the Onset of the Missile Era
- Transitioning from the Supersonic to the Hypersonic: X-7 to X-15
- The Tiles Become Operational
- Shuttle Aerodynamics and Structures
- Aerospaceplane to NASP: The Lure of Air-Breathing Hypersonics
- Transatmospherics after NASP
- Physical Problems, Challenges, and[ Pragmatic Solutions
- Flight Control Systems and Their Design
- Resolving the Challenge of Aerodynamic Damping
- The Challenge of Limit-Cycles
- Flight Control Systems and Pilot-Induced Oscillations
- Self-Adaptive Flight Control Systems
- Induced Structural Resonances
- Fly-By-Wire: Fulfilling Promise and Navigating Around Nuance
- The Advent of Digital Flight Control Systems
- Enhanced Electrical Actuators: Critical Enablers for FBW/DFBW
- Load Feedback for Flight Controls: Imitating the Birds
- Structures and their Aeroelastic Manifestations
- Flutter: The Insidious Threat
- Elastic Aerostructural Effects
- The Advent of Fixed-Base Simulation
- Updating Simulator Prediction with Flight-Test Experience
- Moving Base Cockpit and Centrifuge Simulators
- Variable Stability Airplanes
- Low L/D Approach and Landing Trainers
- Digital Computer Simulation
- Dynamic Instabilities
- Flight Control Coupling
- Dutch Roll Coupling
- Configuration Influence upon Stall and Departure Behavior
- Aerothermodynamics: Meeting the Heating Challenge
- Heat-Sink Structures
- Ablation Cooling
- Hot Structure Approaches
- Lightweight Ceramic Tiles
- Active Cooling Approaches
- NASA and the Evolution of Computational Fluid Dynamics
- The Evolution of Fluid Dynamics from da Vinci to Navier-Stokes
- Computational Fluid Dynamics: What It Is, What It Does
- The Concept of Finite Differences Enters the Mathematical Scene
- The Critical Tool: Emergent High-Speed Electronic Digital Computing
- Some Seminal Solutions and Applications
- The Supersonic Blunt Body Problem
- CFD and Transonic Airfoils
- Navier-Stokes CFD Solutions