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Aircraft
•
Hypersonic
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keywords:(Hypersonic Aircraft)
Active Control of Aerothermoelastic Effects for a Conceptual Hypersonic Aircraft
Activities Report in Aerospace Research in Germany, F.R
Advanced Aeropropulsion Controls Technology
Advanced Airbreathing Hydrocarbon-Fueled Aero-Engine Concepts
Advanced Aircraft Fuel System Simulator Modification and Performance Report
Advanced Air Vehicles Program: Advancing Research in Hypersonic Flight
Advanced Hypersonic Aircraft Design
Advanced Vehicle Concepts Systems and Design Analysis Studies
Advanced X-15A-2 Ablation System Design, Tests, and Analysis
Advances on Propulsion Technology for High-Speed Aircraft. Volume 1
Advances on Propulsion Technology for High-Speed Aircraft. Volume 2
Aeroacoustics of Advanced Propellers
Aerodynamic Analysis of Hypersonic Waverider Aircraft
Aerodynamic Characteristics at Mach 6 of a Wing-Body Concept for a Hypersonic Research Airplane
Aerodynamic Characteristics, Including Effect of Body Shape, of a Mach 6 Aircraft Concept
Aerodynamic Deployable Decelerator Performance-Evaluation Program Phase II
Aerodynamic Design of a Variable-Bend Vehicle
Aerodynamic Heating Measurements on Hypersonic Flight Exoerunebt (HYFLEX) Vehicle
Aerodynamic Maneuvering Hypersonic Flight Mechanics
Aerodynamic Performance Analysis of the Hypersonic Airbreathing Vehicle JAPHAR
Aerodynamic Prediction Techniques for Hypersonic Configuration Design
Aerodynamics of a Mach 7 Powered Aircraft
Aeronautical Research in the United States: Challenges for the 1990's
Aeroservoelastic Stabilization Techniques for Hypersonic Flight Vehicles
Aerospace 2020. Volume 2 - Main Report
Aerospace 2020. Volume 3 - Background Papers
Aerospace Plane Technology: Research and Development Efforts in Europe
Aerospace Plane Technology, Research and Development Efforts in Europe
Aerospace Plane Technology: Research and Development Efforts in Japan and Australia
Aerothermal Flexible Mode Analysis of a Hypersonic Vehicle (Postprint)
Aerothermodynamics Research at NASA AMES
Aerothermodynamic Testing and Boundary Layer Trip Sizing of the HIFiRE Flight 1 Vehicle
A Feasibility Study of Heat-Pipe-Cooled Leading Edges for Hypersonic Cruise Aircraft
Affordable Flight Demonstration of the GTX Air-Breathing SSTO Vehicle Concept
A Fuselage/Tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles: Structural Analysis
A Fuselage/Tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles, Summary
AGARD (Advisory Group for Aerospace Research and Development) Highlights 89/2
Agenda of the Annual Summer Conference (4th), NASA/USRA University Advanced Design Program