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title: AIAA international space planes and hypersonic systems and technologies conference
X-43D Conceptual Design and Feasibility Study
X-43A Fluid and Environmental Systems: Ground and Flight Operation and Lessons Learned
X-43A Flight-Test-Determined Aerodynamic Force and Moment Characteristics at Mach 7.0
Working Process Organization in Rocket-Ramjet with Air Liquefaction Cycle
Understanding Scramjet Combustion using LES of the HyShot II Combustor (AIAA 2015-3615)
Understanding Scramjet Combustion using LES of the HyShot II Combustor
Turboramjet Propulsion for Hypersonic Booster-Aircraft of TSTO Aerospace System
TSTO Airbreathing Propulsion Analysis with Lift and Drag
Trajectory Planning for Cooperative Flight of Two Hypersonic Entry Vehicles (AIAA 2017-2251)
Trajectory Planning for Cooperative Flight of Two Hypersonic Entry Vehicles
Trajectory Design of a Rocket-Scramjet-Rocket Multi-Stage Launch System (AIAA 2017-2107)
Trajectory and Guidance Scheme Design for Free Flight Test of Hypersonic Vehicle (AIAA 2017-2197)
Trajectory and guidance scheme design for free flight test of hypersonic vehicle
Thrust modeling for hypersonic engines
The X-43A Hyper-X Mach 7 Flight 2 Guidance, Navigation, and Control Overview and Flight Test Results