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Full Length Papers(Scramjet)(2013)
2013・X-51A Scramjet Demonstrator Program: Waverider Ground And Flight Test
・OVERVIEW OF THE SCRAMJET COMBUSTION CHAMBER LENGTH
・DEVELOPMENT AND OPERATION OF AN INTEGRATED SAMPLING PROBE AND GAS ANALYZER FOR TURBULENT MIXING STUDIES IN COMPLEX SUPERSONIC FLOWS
・Methane Pyrolysis: literature survey and comparisons of available data for use in numerical simulations
・Aerothermodynamics & Turbulence
・Theoretical analysis of effects of boundary layer bleed on scramjet thrust
・Implementation of Implicit Adaptive Mesh Re nement in an Unstructured Finite-Volume Flow Solver
・Nonequilibrium Plasma-Assisted Combustion:A Review of Recent Progress
・Numerical simulations of supersonic combustion experiments for scramjet propulsion in the ONERA F4 hypersonic wind tunnel
・STUDY OF AN AIR-BREATHING ENGINE FOR HYPERSONIC FLIGHT
・Thermal Management at Hypersonic Leading Edges
・Numerical Studies on Flow Field Characteristics of Cavity Based Scramjet Combustors
・Effects of Leading-Edge Truncation and Stunting on Drag and Efficiency of Busemann Intakes for Axisymmetric Scramjet Engines
・(JOURNAL OF PROPULSION AND POWER, Vol. 29, No. 3, May-June 2013)Effects of Sidewall Compression and Relaminarization in a Scramjet Inlet
・Effect of Homogeneous Condensation on the Interaction of Supersonic Moist Air Jets with Resonance Tube
・A parameterized geometry design method for inward turning inlet compatible waverider
・Interactions between Flight Dynamics and Propulsion Systems of Air-Breathing Hypersonic Vehicles
・Nonequilibrium Plasma-Assisted Combustion:A Review of Recent Progress
・Dual-pump CARS of Air in a Heated Pressure Vessel up to 55 Bar and 1300 K
・(AIAA2013-2810)Planar Laser-Induced Fluorescence Velocity Measurements of Retropropulsion Jets in a Mach 12 Freestream
・(AIAA2013-2606)Hypersonics Into the 21st Century: A Perspective on AFOSR-Sponsored Research in Aerothermodynamics
・(AIAA2013-1457)Structural Response and Service Life Prediction Concerns in the Design of Hypersonic Flight Vehicle Hot Structure
・(AIAA2013-0696)Measurements on NASA Langley Durable Combustor Rig by TDLAT: Preliminary Results
・(AIAA2013-0685)Recalibration of the Shear Stress Transport Model to Improve Calculation of Shock Separated Flows
・(AIAA2013-0375)Hypersonic Boundary-Layer Transition Experiments in the Boeing/AFOSR Mach-6 Quiet Tunnel
・(AIAA2013-0335)Dual-Pump CARS Measurements in the University of Virginia's Dual-Mode Scramjet: Configuration “C”
・(AIAA2013-0271)Hypersonic boundary-layer stabilization by means of ultrasonically absorptive carbon-carbon material - Part 2: Computational Analysis
・(AIAA2013-0270)Hypersonic boundary-layer stabilization by means of ultrasonically absorptive carbon-carbon material Part 1: Experimental Results
・(AIAA2013-0117)Continued Hybrid LES / RANS Simulation of a Hypersonic Dual-Mode Scramjet Combustor
・(AIAA2013-0084)Instability and Transition due to Near-Critical Roughness in a Hypersonic Laminar Boundary Layer
・(AIAA2013-0081)Wake Instabilities behind Discrete Roughness Elements in High Speed Boundary Layers
・(AIAA2013-0034)OH PLIF Visualization of the UVa Supersonic Combustion Experiment: Configuration C