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journal:(8th AIAA Atmospheric and Space Environments Conference)
Weber Number Tests in the NASA Icing Research Tunnel (AIAA 2018-3184)
Use of Simple Models to Determine Wake Vortex Categories for New Aircraft (Invited) (AIAA 2015-3172)
The Investigation of Operation Domain of Strut Fuel Feed System for Model Scramjet Combustor
The FESTIP Technology Development and Verification Plan
The Adhesion Strength of Impact Ice Measured Using a Modified Lap Joint Test (AIAA 2018-3341)
Testing of Elastomer Icephobic Coatings (AIAA 2018-3656)
Summary of Ice Shape Geometric Fidelity Studies on an Iced Swept Wing (AIAA 2018-3494)
Some Numerical Investigation Results of Shock-Induced Combustion
Simulation Tests for Investigating Flying Qualities of Aerospace Planes
Simulations of Orographic Flows Using Unstructured and Structured Meshes (Invited) (AIAA 2015-2891)
Simulation of Atomization Equipment in Icing Cloud Simulation System (AIAA 2018-3651)
Sensor Suite Development for a Weather UAV (AIAA 2015-3022)
Sensitivity Analysis of Wake Vortex Parameters Measured by Doppler Lidar (AIAA 2015-3023)
Sensitivity Analysis of Aircraft Encounters with Deformed Wake Vortices (Invited) (AIAA 2015-3175)
Scramjet Combustor Design in French PREPHA Program - Final Status in 1998
Rotor Ice Shedding and Trajectory Analyses in Forward Flight (AIAA 2018-3659)
Ride Quality Within Trail Aircraft In Formation Flight (AIAA 2015-3325)
Reynolds Number Effects on the Low-speed Aerodynamics of the Hypersonic Configuration ELAC-1
Reusable Launchers Tank Structures: Requirements Definition and Experimental Development
Results for a Fully Reusable TSTO-Launch Vehicle Concept
Resonant Holographic Interferometry Measurements of OH Distribution in a Hypersonic Reacting Flow
Recent Advances in Wind Lidar Technologies for Characterization of Wake Vortices (AIAA 2018-2863)
Ramjet Engine Test Facility (RJTF) in NAL-KRC, Japan
Quasi-Unsteady Icing Simulation of an Oscillating Airfoil (AIAA 2015-3020)
Progress in SSTO and TSTO Aerospace Plane Combined Propulsion System Research Program ("ORYOL-2-1")
Perspectives of International Cooperation in the Spaceplane Sector
Performance of Centrospazio Hypersonic High Enthalpy Wind Tunnel
Pegasus Wing-Glove Experiment to Document Crossflow Transition - Development and Current Status
Particle Size Calibration Testing in the NASA Propulsion System Laboratory (AIAA 2018-3971)
Optimizing Hypersonic Sharp Body Concepts from a Thermal Protection System Perspective
Optimization of a Space Transportation System Including Design Sensitivities
Oblique Detonation Wave Studies in the Caltech T-5 Shock Tunnel Facility