Relevant bibliographies by topics / Hypersonic Vehicle

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Hypersonic Vehicle'

Author: Grafiati
Published: 4 June 2021
Last updated: 13 June 2025

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Journal articles on the topic "Hypersonic Vehicle"

1

Haley, J. G., T. P. McCall, I. W. Maynard, and B. Chudoba. "A sizing-based approach to evaluate hypersonic demonstrators: demonstrator-carrier constraints." Aeronautical Journal 124, no. 1279 (2020): 1318–49. http://dx.doi.org/10.1017/aer.2020.30.

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ABSTRACTThe objective of this study is to identify, evaluate, and provide recommendations towards the realisation of near-term hypersonic flight hardware through the consideration of carrier vehicle constraints. The current rush of available funds for hypersonic research cannot cause a program to ignore growth potential for future missions. The prior NB-52 carrier vehicles, famous for the X-15 and X-43A missions, are retired. Next generation hypersonic demonstrator requirements will necessitate a substitution of carrier vehicle capability. Flight vehicle configuration, technology requirements,
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de Araujo Martos, João Felipe, Israel da Silveira Rêgo, Sergio Nicholas Pachon Laiton, Bruno Coelho Lima, Felipe Jean Costa, and Paulo Gilberto de Paula Toro. "Experimental Investigation of Brazilian 14-X B Hypersonic Scramjet Aerospace Vehicle." International Journal of Aerospace Engineering 2017 (2017): 1–10. http://dx.doi.org/10.1155/2017/5496527.

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The Brazilian hypersonic scramjet aerospace vehicle 14-X B is a technological demonstrator of a hypersonic airbreathing propulsion system based on the supersonic combustion (scramjet) to be tested in flight into the Earth’s atmosphere at an altitude of 30 km and Mach number 7. The 14-X B has been designed at the Prof. Henry T. Nagamatsu Laboratory of Aerothermodynamics and Hypersonics, Institute for Advanced Studies (IEAv), Brazil. The IEAv T3 Hypersonic Shock Tunnel is a ground-test facility able to produce high Mach number and high enthalpy flows in the test section close to those encountere
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Gao, Mengjing, Tian Yan, Quancheng Li, Wenxing Fu, and Jin Zhang. "Intelligent Pursuit–Evasion Game Based on Deep Reinforcement Learning for Hypersonic Vehicles." Aerospace 10, no. 1 (2023): 86. http://dx.doi.org/10.3390/aerospace10010086.

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As defense technology develops, it is essential to study the pursuit–evasion (PE) game problem in hypersonic vehicles, especially in the situation where a head-on scenario is created. Under a head-on situation, the hypersonic vehicle’s speed advantage is offset. This paper, therefore, establishes the scenario and model for the two sides of attack and defense, using the twin delayed deep deterministic (TD3) gradient strategy, which has a faster convergence speed and reduces over-estimation. In view of the flight state–action value function, the decision framework for escape control based on the
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Zhong, Qin, and Wenbin Wu. "A Switching-Based Interference Control for Booster Separation of Hypersonic Vehicle." Wireless Communications and Mobile Computing 2021 (December 15, 2021): 1–9. http://dx.doi.org/10.1155/2021/2115641.

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Whether launching from the ground or in the air, hypersonic vehicles need the booster to accelerate to a predetermined window, so as to meet the requirements of scramjet engine ignition. Therefore, there is interference suppression between boosters and hypersonic vehicles under the high dynamic pressure, which has become a key technical problem that affects the success of flight tests, especially when the aircraft is statically unstable. A method of variable structure switching-based control is proposed in this paper for rapid suppression on hypersonic vehicle booster separation interference.
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Lu, Hai Bo, and Wei Qiang Liu. "Aerodynamic Investigation of Hypersonic Vehicle with Forward-Facing Cavity." Applied Mechanics and Materials 108 (October 2011): 41–47. http://dx.doi.org/10.4028/www.scientific.net/amm.108.41.

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Forward-facing cavity mounted on the blunt nose of hypersonic vehicle is a good choice to reduce the stagnation heating. Presently, the study on hypersonic vehicles nose tip with forward-facing cavity mainly focus on its thermology characteristic, and little work can be found investigating the effect of cavity on aerodynamic force for a holistic vehicle. The CFD method is developed to investigate the effect of cavity geometry on aerodynamic performance of hypersonic vehicle with a forward-facing cavity on the nose-tip. Drag coefficient, lift coefficient and pitching moment coefficient of the v
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Balakin, V. L., and M. M. Krikunov. "Disturbed motion of a hypersonic vehicle in climb." VESTNIK of Samara University. Aerospace and Mechanical Engineering 18, no. 2 (2019): 7–20. http://dx.doi.org/10.18287/2541-7533-2019-18-2-7-20.

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Disturbed motion of a hypersonic vehicle in climb is analyzed. Deviations of atmospheric density from standard values and deviations of aerodynamic force coefficients from nominal values are taken as disturbances. Disturbed motion of a hypersonic vehicle with the optimum angle-of-attack schedule and nominal flight characteristics is modeled. Deviations of terminal conditions of disturbed motion from the target values of velocity, altitude and path inclination are determined. Using the method of Pontryagin’s maximum principle the problem of fuel mass minimum consumed in hypersonic acceleration
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Cheng, Yunpeng, Xiaodong Yan, and Feng Cheng. "Trajectory Estimation of Hypersonic Glide Vehicle Based on Analysis of Aerodynamic Performance." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 37, no. 6 (2019): 1102–10. http://dx.doi.org/10.1051/jnwpu/20193761102.

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Due to high speed and high maneuverability of hypersonic glide vehicles (HGVs), the state estimation of such targets has always been a research hotspot. In order to improve accuracy of the trajectory estimation, a nonlinear aerodynamic parameter model for target estimation based on aerodynamic performance analysis is proposed. Firstly, the dynamic characteristics of the hypersonic glide vehicle during the hypersonic gliding stage was analyzed. Then, aiming at HTV-2-liked vehicle, the engineering calculation method was used to form the reference aerodynamic model for the target estimation. Seco
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Yin, Xiaomeng, Xinming Li, Lei Liu, Yongji Wang, and Xing Wei. "A probabilistic robust mixed H2/H∞ fuzzy control method for hypersonic vehicles based on reliability theory." International Journal of Advanced Robotic Systems 15, no. 1 (2018): 172988141775415. http://dx.doi.org/10.1177/1729881417754153.

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Achieving balance between robustness and performance is always a challenge in the hypersonic vehicle flight control design. In this research, we focus on dealing with uncertainties of the fuzzy control system from the viewpoint of reliability. A probabilistic robust mixed H2/ H∞ fuzzy control method for hypersonic vehicles is presented by describing the uncertain parameters as random variables. First, a Takagi–Sugeno fuzzy model is employed for the hypersonic vehicle nonlinear dynamics characteristics. Next, a robust fuzzy controller is developed by solving a reliability-based multi-objective
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9

Blankson, I. M. "Air-Breathing Hypersonic Cruise: Prospects for Mach 4–7 Waverider Aircraft." Journal of Engineering for Gas Turbines and Power 116, no. 1 (1994): 104–15. http://dx.doi.org/10.1115/1.2906779.

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There is currently a renewal of world-wide interest in hypersonic flight. Vehicle concepts being considered range from cruise missiles to SSTO and TSTO vehicles. The new characteristics of these vehicles are that they will be powered by air-breathing engines and have long residence times in the air-breathing corridor. In the Mach 4–7 regime, waverider aircraft are being considered as candidates for both long-range and short-range cruise missions, as hypersonic missiles, and as high-L/D highly maneuverable vehicles. This paper will discuss the potential for near-term and far-term application of
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Liang, Bingbing, Ziyang Zhen, and Ju Jiang. "Modified shuffled frog leaping algorithm optimized control for air-breathing hypersonic flight vehicle." International Journal of Advanced Robotic Systems 13, no. 6 (2016): 172988141667813. http://dx.doi.org/10.1177/1729881416678136.

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This article addresses the flight control problem of air-breathing hypersonic vehicles and proposes a novel intelligent algorithm optimized control method. To achieve the climbing, cruising and descending flight control of the air-breathing hypersonic vehicle, an engineering-oriented flight control system based on a Proportional Integral Derivative (PID) method is designed for the hypersonic vehicle, which including the height loop, the pitch angle loop and the velocity loop. Moreover, as a variant of nature-inspired algorithm, modified shuffled frog leaping algorithm is presented to optimize
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Dissertations / Theses on the topic "Hypersonic Vehicle"

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Haq, Z. U. "Hypersonic vehicle interference heating." Thesis, University of Southampton, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.336171.

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Wiese, Daniel Philip. "Adaptive control of a generic hypersonic vehicle." Thesis, Massachusetts Institute of Technology, 2013. http://hdl.handle.net/1721.1/81714.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2013.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (p. 111-115).<br>This thesis presents a an adaptive augmented, gain-scheduled baseline LQR-PI controller applied to the Road Runner six-degree-of-freedom generic hypersonic vehicle model. Uncertainty in control effectiveness, longitudinal center of gravity location, and aerodynamic coefficients are introduced in the model, as well as sensor bias and noise, and input time delays. The performance of the baseline controller is
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Morimoto, Hitoshi. "Trajectory optimization for a hypersonic vehicle with constraint." Diss., Georgia Institute of Technology, 1997. http://hdl.handle.net/1853/12076.

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Modlin, James Michael. "Hypersonic aerospace vehicle leading edge cooling using heat pipe, transpiration and film cooling techniques." Diss., Georgia Institute of Technology, 1991. http://hdl.handle.net/1853/16347.

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Janicki, William D. (William Daniel). "Asymptotic analysis of hypersonic vehicle dynamics along entry trajectory." Thesis, Massachusetts Institute of Technology, 1991. http://hdl.handle.net/1721.1/42502.

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DiGregorio, Nicholas J. "Characteristics of Turbulent Boundary Layers along a Hypersonic Vehicle." Thesis, State University of New York at Buffalo, 2018. http://pqdtopen.proquest.com/#viewpdf?dispub=10822170.

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<p> The flight conditions of a hypersonic vehicle on an ascent trajectory are computed and Reynolds-averaged Navier-Stokes (RANS) simulations of the turbulent boundary layers are performed across a Mach number range of 0.3 up to 16 using the computational fluid dynamics (CFD) software, VULCAN. The boundary conditions and leading edge geometry are varied from the simple case of adiabatic and sharp to cooled and blunted to reveal the physics of how these effects impact the results of flat plate boundary layer methods as applied to practical aerospace systems. The law of the wall, the Van Driest
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Sudalagunta, Praneeth Reddy. "Control-oriented Modeling of an Air-breathing Hypersonic Vehicle." Diss., Virginia Tech, 2016. http://hdl.handle.net/10919/72872.

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Design and development of future high speed aircraft require the use of advanced modeling tools early on in the design phase to study and analyze complex aeroelastic, thermoelastic, and aerothermal interactions. This phase, commonly referred to as the conceptual design phase, involves using first principle based analytical models to obtain a practical starting point for the preliminary and detailed design phases. These analytical models are expected to, firstly, capture the effect of complex interactions between various subsystems using basic physics, and secondly, minimize computational costs
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Choi, June. "Application of hypersonic vehicle flying qualities criteria and computational considerations." Thesis, Massachusetts Institute of Technology, 1994. http://hdl.handle.net/1721.1/47356.

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Araki, John Jun. "Reentry dynamics and handling qualities of a generic hypersonic vehicle." Thesis, Massachusetts Institute of Technology, 1992. http://hdl.handle.net/1721.1/42532.

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Camillo, Giannino Ponchio. "Longitudinal stability analysis and control of an airbreathing hypersonic vehicle." Instituto Tecnológico de Aeronáutica, 2014. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3154.

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This work presents the open-loop stability analysis and an active control strategy for an airbreathing hypersonic vehicle. The 14-XB, a bidimensional flow airframe derived from the Brazilian 14-X Aerospace Hypersonic Vehicle, is adopted as study platform. In order to perform such analyses, a simulation mathematical model of the airframe longitudinal forces and moments is obtained using perfect gas equations, after considering the relevance of the real gas hypotheses for the expected Mach number range and verifying that the simpler formulation is sufficient. An all-moving horizontal tail is des
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Books on the topic "Hypersonic Vehicle"

1

Baysal, Oktay. Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle. Langley Research Center, 1992.

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Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-8901-0.

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Baysal, Oktay. Flow analysis and design optimization methods for nozzle after body of a hypersonic vehicle. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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B, Murphy S. N., and Curran E. T, eds. Developments in high-speed-vehicle propusion systems. American Institute of Aeronautics and Astronautics, Inc., 1996.

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Harris, Elwyn D. The national aerospace plane: Cost considerations for the follow-on vehicle. RAND, 1994.

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Iliff, Kenneth W. A comparison of hypersonic vehicle flight and prediction results. National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.

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Flandro, G. A. Dynamic interactions between hypersonic vehicle aerodynamics and propulsion system performance: Final report to Aircraft Guidance and Controls Branch, Guidance and Control Division ... National Aeronautics and Space Administration, 1992.

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Gregory, Irene M. Hypersonic vehicle model and control law development using H and u synthesis. Langley Research Center, 1994.

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Messitt, D. G. Comparison between computational and experimental data for a hypersonic laser propelled vehicle. American Institute of Aeronautics and Astronautics, 1992.

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Riehl, John. SRM-assisted trajectory for the GTX reference vehicle. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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Book chapters on the topic "Hypersonic Vehicle"

1

Hunt, James L. "Hypersonic Airbreathing Vehicle Design (Focus on Aero-Space Plane)." In Hypersonics. Birkhäuser Boston, 1989. http://dx.doi.org/10.1007/978-1-4684-9187-6_5.

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Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. "Mathematical Modeling for Hypersonic Glide Problem." In Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-8901-0_3.

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Chudej, Kurt. "Optimal Ascent of a Hypersonic Space Vehicle." In Optimal Control. Birkhäuser Basel, 1993. http://dx.doi.org/10.1007/978-3-0348-7539-4_23.

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Hughes, Hunter D., and Fen Wu. "LPV H∞ Control for Flexible Hypersonic Vehicle." In Control of Linear Parameter Varying Systems with Applications. Springer US, 2012. http://dx.doi.org/10.1007/978-1-4614-1833-7_16.

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Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. "Singular Perturbation Guidance of Hypersonic Glide Reentry." In Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-8901-0_11.

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da Cunha Follador, Roberto, Andrea de Oliveira Netto Follador, Paloma Ribeiro dos Santos, and Geilson Loureiro. "Systems Concurrent Engineering of a Hypersonic Accelerator Vehicle." In Advanced Concurrent Engineering. Springer London, 2011. http://dx.doi.org/10.1007/978-0-85729-799-0_6.

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Li, Le-yao, Xin-min Wang, and Ling-xia Mu. "Incipient Fault Detection for a Hypersonic Scramjet Vehicle." In Proceedings of the First Symposium on Aviation Maintenance and Management-Volume I. Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54236-7_4.

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Hirschel, Ernst Heinrich, and Claus Weiland. "The Thermal State of a Hypersonic Vehicle Surface." In Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-89974-7_9.

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Zhang, Zhiyao, Tieshan Feng, Zongzhun Zheng, Hao Wu, and Yun Tan. "Fuzzy Active Disturbance Rejection Control for Hypersonic Vehicle." In Lecture Notes in Electrical Engineering. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-8155-7_210.

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Ma, Xianlong, Weijun Hu, and Zhiqiang Gao. "Hypersonic Vehicle Control Based on Deep Reinforcement Learning." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-19-7652-0_6.

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Conference papers on the topic "Hypersonic Vehicle"

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Pulok, Mohammad Khairul Habib, and Uttam K. Chakravarty. "Aerodynamic and Vibration Analysis of the Morphing Wings of a Hypersonic Vehicle." In ASME 2020 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/imece2020-23663.

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Abstract Hypersonic vehicles are receiving great attention in recent years due to their high speed and long-range capabilities. The shock waves come into consideration as a propagating disturbance for any aircraft when it exceeds the speed of sound. Complex environment and flight requirements of the hypersonic vehicles are leading the researchers to focus on several design considerations. Adaptive shape deformation is one of the prospective areas among them which has an impact on thermal loading, global and local load factors, vehicle acceleration, total energy dissipation, and fuel consumptio
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Markell, Kyle C., Keith M. Brewer, and Michael R. von Spakovsky. "Exergy Methods Applied to the Integrated Mission-Level Analysis and Optimization of Hypersonic Vehicle Concepts." In ASME 2007 International Mechanical Engineering Congress and Exposition. ASMEDC, 2007. http://dx.doi.org/10.1115/imece2007-42938.

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The results of the application of an exergy-based method to highly dynamic, integrated hypersonic vehicle concepts are presented. Conventional aircraft systems and sub-systems traditionally are designed relying heavily on rules of thumb, individual experience, and rather simple, non-integrated tradeoff analyses, which are highly dependent on the evolutionary nature of vehicle development. In contrast, hypersonic vehicles may contain new sub-systems and revolutionary concepts for which there is no existing database to support an evolutionary synthesis/design approach. Thus, a simple tradeoff an
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Bez, Jean-Pierre, Jean-Jacques Chattot, and Francois Noel. "Some Validations by Experimental Results in Hypersonic Flow Computations." In Aerospace Vehicle Conference. SAE International, 1988. http://dx.doi.org/10.4271/880925.

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Blankson, Isaiah M. "Air-Breathing Hypersonic Cruise: Prospects for Mach 4-7 Waverider Aircraft." In ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/92-gt-437.

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There is currently a renewal of world-wide interest in hypersonic flight. Vehicle concepts being considered range from cruise missiles to SSTO and TSTO vehicles. The new characteristics of these vehicles are that they will be powered by air-breathing engines and have long residence times in the air-breathing corridor. In the Mach 4-7 regime, waverider aircraft are being considered as candidates for both long-range and short-range cruise missions, as hypersonic missiles, and as high L/D highly maneuverable vehicles. This paper will discuss the potential for near-term and far-term application of
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HANEY, J., R. CERVISI, A. GRANTZ, and T. SMITH. "A hypersonic waverider research vehicle." In 31st Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-402.

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Lazur, Andrew, J. Sawyer, Brian Sullivan, and Larry Hudson. "Hypersonic vehicle control surface development." In 9th International Space Planes and Hypersonic Systems and Technologies Conference. American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-4864.

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Haley, James, and Bernd Chudoba. "Hypersonic Vehicle Solution Space Screening." In 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-5316.

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HERRLIN, JACK, and HENDRIK GELDERLOOS. "Vehicle management system for a manned hypersonic vehicle." In Digital Avionics Systems Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3877.

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Kremer, Frans G. J. "Balance of Moments for Hypersonic Vehicles." In ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/92-gt-251.

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Ramjet engines propelling hypersonic flight vehicles will be highly integrated into the vehicle, resulting in strong interactions between the vehicle and the engine. An assessment of these interactions in relation to the flight mission is made by simple but adequate modeling of the flight vehicle aerodynamics and the engine performance. Especially moments associated with the propulsion system are of interest. This paper deals with the pitch moments introduced by the ramjet related forces, which are evaluated by one-dimensional engine performance and by modeling of the inlet and nozzle flow. Fu
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"The Hypersonic PreX Vehicle: Current Status." In 55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.iac-04-v.6.07.

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Reports on the topic "Hypersonic Vehicle"

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Tandon, Rajan, Hans Peter Dumm, Erica L. Corral, Ronald E. Loehman, and Paul Gabriel Kotula. Ultra high temperature ceramics for hypersonic vehicle applications. Office of Scientific and Technical Information (OSTI), 2006. http://dx.doi.org/10.2172/887260.

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Spravka, John J., and Timothy R. Jorris. Current Hypersonic and Space Vehicle Flight Test and Instrumentation. Defense Technical Information Center, 2015. http://dx.doi.org/10.21236/ada619521.

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Groves, Kevin P., Andrea Serrani, Stephen Yurkovich, Michael A. Bolender, and David B. Doman. Anti-Windup Control for an Air-Breathing Hypersonic Vehicle Model. Defense Technical Information Center, 2005. http://dx.doi.org/10.21236/ada444973.

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Huynh, Thomas, and Joseph Kriz. Final Environmental Assessment for Hypersonic Technology Vehicle 2 Flight Tests. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada640309.

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McGrory, William D. Hypersonic Maneuvering Vehicle Simulations Using Real-Gas, Unstructured Navier-Stokes Software. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada399497.

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Olguin, Abel. Technical and Programmatic Consequences of a Hypersonic Vehicle Flight Test Ban. Office of Scientific and Technical Information (OSTI), 2019. http://dx.doi.org/10.2172/1630998.

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Chen, Ping-Chih, Ryan Starkey, Kai-Ti Chang, and Ayan Sengupta. Integrated Aero-Servo-Thermo-Propulso-Elasticity (ASTPE) for Hypersonic Scramjet Vehicle Design/Analysis. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada590178.

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Liu, D. D., P. C. Chen, Lei Tang, K. T. Chang, and Adel Chemaly. Integrated Hypersonic Aerothermoelastic Methodology for Transatmospheric Vehicle (TAV)/Thermal Protection System (TPS) Structural Design and Optimization. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada403577.

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Kimmel, Roger, David Adamczak, Ryan Gosse, Karen Berger, and Shann Rufer. Ground Test and Computation of Boundary Layer Transition on the Hypersonic International Flight Research and Experimentation (HIFiRE)-5 Vehicle. Defense Technical Information Center, 2011. http://dx.doi.org/10.21236/ada548272.

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Saalman, Lora. Multidomain Deterrence and Strategic Stability in China. Stockholm International Peace Research Institute, 2022. http://dx.doi.org/10.55163/fyxq3853.

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Over the past few years, China has displayed a wide range of advances in military capabilities and infrastructure, including its test of a hypersonic glide vehicle coupled with a fractional orbital bombardment system and evidence of new intercontinental ballistic missile silos. While China and the United States remain at political odds, there are indications that China’s strategies in space, cyberspace and nuclear domains are increasingly converging with those of the USA, as well as Russia. A key question is whether this strategic convergence is a stabilizing or destabilizing phenomenon. To an
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