1–50 von 109 Ergebnissen
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    A concept and flight testing of fully reusable rocket vehicle

    Inatani, Yoshifumi / Naruo, Yoshihiro / Yonemoto, Koich | AIAA | 1999
    Verlag: The American Institute of Aeronautics and Astronautics

    Advanced Simulations of Reusable Hypersonic Rocket-Powered Stages

    Sippel, Martin / Bussler, Leonid / Kopp, Alexander | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Aerodynamic configuration design and optimization for hypersonic vehicles

    Feng, Yi / Liu, Shenshen / Tang, Wei et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Aerodynamic Performance Analysis of A New Conception Hypersonic Aircraft

    Ma, Xiaoyong / Zhong, Shidong / Xiao, Yu et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Airbreather/Rocket Combined Cycle (ARCC) engine for spaceplanes

    Yamanaka, T. / Ohkoshi, H. / Maita, M. et al. | AIAA | 1999
    Verlag: The American Institute of Aeronautics and Astronautics

    Airbreather/rocket combined propulsion system research for Japanese SSTO spaceplane

    Taguchi, Hideyuki / Maita, Masataka / Yatsuyanagi, Nobuyuki et al. | AIAA | 1999
    Verlag: The American Institute of Aeronautics and Astronautics

    Airbreathing Hypersonic Propulsion at Pratt & Whitney - Overview

    Kazmar, Richard | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics

    Airbreathing hypersonic propulsion system integration within FESTIP FSSC-12

    Kopp, Sven / Hollmeier, Sebastian / Rick, Hans et al. | AIAA | 1999
    Verlag: The American Institute of Aeronautics and Astronautics

    Airbreathing hypersonic systems focus at NASA Langley Research Center

    Hunt, James / Rausch, Vincent | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    An airbreathing launch vehicle design with turbine-based lowspeed propulsion and dual mode scramjet high-speed propulsion

    Moses, P. / Bouchard, K. / Vause, R. et al. | AIAA | 1999
    Verlag: The American Institute of Aeronautics and Astronautics

    Analysis of longitudinal dynamic characteristics for air-breathing hypersonic flight vehicle

    Li, Yongtao / Wu, Yu / Tan, Wenqian et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Analysis of the Stability and Chattering Effects of Sliding Mode Control for Hypersonic Vehicles

    Li, Renfu / Zhang, Yuanyuan / Liu, Zhimin | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    An Efficient Flamelet-based Combustion Model for Supersonic Flows

    Saghafian, Amirreza / Terrapon, Vincent / Ham, Frank et al. | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    An Efficient Integrated Aerothermoelasticity Analysis System Based on Surrogate-based Reduced Order Modeling for Hypersonic Vehicles

    Chen, Xin / Zuo, Guang / Shi, Yong et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    A New Aerodynamic Layout for Large-scale Conventional Hypersonic Wind Tunnel

    Wang, Tiejin | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    A Preliminary Research on a Two-Stage-To-Orbit Vehicle with Airbreathing Pre-cooled Hypersonic Engines

    Zhou, Jianxing / Lu, Hong / Zhang, Haocheng et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    A Rapid Aerodynamics/Propulsion Analysis Method for Hypersonic Flight Vehicle MDO

    Gong, Chunlin / Yuan, Jianping / Gu, Liangxian et al. | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    A Review of Uncertainty Analysis for Hypersonic Inflatable Aerodynamic Decelerator Design

    Brune, Andrew J. / West, Thomas / Hosder, Serhat et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    A Unified Angle Control Scheme for Hypersonic Vehicle Based on Disturbance Rejection

    Piao, Minnan / Zhu, Kai / Sun, Mingwei et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    CFD Calculations for Intake-Injection Shock-Induced-Combustion Scramjet Flight Experiments

    Mudford, Neil / Mulreany, Peter / McGuire, Jeffrey et al. | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    CFD Results of Ignition Enhancement for Scramjet Combustion

    McGuire, Jeffrey / Boyce, Russell / Mudford, Neil | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    CFD Simulations for AEDC Combustion Air Heater (CAH) for APTU Facility

    Ebrahimi, Houshang / Ryder, Robert | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    Characteristics of Supersonic Combustion with Hartmann-Sprenger Tube Aided Fuel Injection

    Gu, Hongbin / Zhi, Li / Chen, Lihong et al. | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    Combustion of hydrogen in hot air flows within LAPCAT-II Dual Mode Ramjet combustor at Onera-LAERTE facility - Experimental and Numerical Investigation

    Vincent-Randonnier, Axel / Moule, Yann / Ferrier, Marc | AIAA | 2014
    Verlag: The American Institute of Aeronautics and Astronautics

    Combustion Regimes in Inlet-fulled, Low Compression Scramjets

    Gehre, Rolf / Wheatley, Vincent / Boyce, Russell | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    Combustor data bases for hypersonic airbreathing propulsion systems

    McDaniel, Jr., James | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    Comparison of VTOL and HTHL Hypersonic Aircrafts

    Xiaopeng, Zhou / Haixin, Chen | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Compartmental Tank Propellant Management System Design and Operation for Hypersonic Vehicle

    Su, Lichao | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Design and performance of a hypersonic quiet wind tunnel at NUDT

    Gang, Dundian / Yi, Shihe / Lu, Xiaoge | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Design Methodology for the Airbreathing Second Stage of a Rocket-Scramjet-Rocket Launch Vehicle

    Jazra, Thomas / Smart, Michael | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    Design of hypersonic forebody by the combination of bump and waverider surfaces

    Saheby, Eiman B. / Huang, Guoping / Hays, Anthony | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Development and capabilities of the NASA Langley Cryogenic Pressure Box

    Glass, David / Blackburn, Charles / Stevens, Jonathan et al. | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    Development of hypersonic wind tunnel free-flight test in CAAA

    Jiang, Zenghui / Song, Wei / Lu, Wei | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Dimensional Expanding Precise Time Integration (DE-PTI) for Transient Heat Transfer Analysis of Thermal Protection Systems

    Zhu, Wenxiang / Liu, Jiawen / Yao, Jianyao et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Disturbance Observer Based Back-Stepping Attitude Control for Flexible Hypersonic Vehicle

    Yueyong, Lv / Wang, Runchi | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    DLR THERMEX-B test facility for cryogenic tank wall structures

    Petersen, D. / Klein, H. / Schmidt, K. | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    Effect of plasma on the ignition and combustion characteristics of boron containing systems

    Zhang, Peng / Ding, Xiaoyu | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Effusion Cooled CMC Rocket Combustion Chamber

    Hald, Hermann / Ortelt, Markus / Fischer, Ingo et al. | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics

    Energy Deposition I: Applications to Revolutionize High Speed Flight and Flow Control

    Kremeyer, Kevin P. | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    Experimental Analysis of 14-X B Hypersonic Aerospace Vehicle Compression System

    Martos, João F. / Toro, Paulo G. de P. / Rego, Israel S. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Experimental Study of Hypersonic Flutter of a Blunt-leading-edge Trapezoidal Wing

    Ji, Chen / Jiang, Wei / Zhu, Jian et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Experimental study on compact heat exchanger for hypersonic aero-engine

    Lee, Huan / Ma, Song / Chen, Yiming et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Exploring Dynamic Characteristics of Steady Turning for Airframe-propulsion Integrated Hypersonic Vehicle

    Li, Yongtao / Tan, Wenqian / Wu, Yu et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Fabrication and testing of a leading-edge-shaped heat pipe

    Glass, David / Camarda, Charles / Merrigan, Michael et al. | AIAA | 1999
    Verlag: The American Institute of Aeronautics and Astronautics

    Flight dynamics and robust control of a hypersonic test vehicle with ramjet propulsion

    Heller, M. / Sachs, G. / Gunnarsson, K. et al. | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    Flight Performance of An Airbreathing Rocket Combuned Engine Powered Spaceplane

    Yamanaka, Tatsuo | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    Flight-Ready TDLAS Combustion Sensor for Hypersonics

    Masterson, Bernard / Sappey, Andrew / Owenby, David et al. | AIAA | 2009
    Verlag: The American Institute of Aeronautics and Astronautics

    Fluid-thermal-structural coupling simulation method under hypersonic heating environment

    Wang, Gang / Qin, Mengzhu / Hong, Liangyou | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Fuel Atomization and Droplet Breakup Models for Numerical Simulation of Spray Combustion in a Scramjet Combustor

    Shunhua, YANG / Jialing, LE / Wei, HE et al. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

    Fundamental Analysis of a Combined Cycle Rocket-Ramjet Propulsion System

    LeMoyne, Robert | AIAA | 2008
    Verlag: The American Institute of Aeronautics and Astronautics