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Developments In High-Speed Vehicle Propulsion Systems
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1115/1.3250615openalex-snapshot
Progress in Turbulent Forced Convection
inferredcites →https://doi.org/10.1115/91-gt-395openalex-snapshot
Propulsion Aspects of Hypersonic Turbo-Ramjet-Engines With Special Emphasis on Nozzle/Aftbody Integration
inferredcites →https://doi.org/10.2514/3.8182openalex-snapshot
Turbulence modeling for computational aerodynamics
inferredcites →https://doi.org/10.2514/6.1995-6005openalex-snapshot
The German Hypersonics Technology Program - Overview
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
inferred← citeshttps://doi.org/10.1007/978-3-540-27009-6_8openalex-snapshot
Some perspectives on pulse detonation propulsion systems
inferred← citeshttps://doi.org/10.1007/978-3-642-25685-1_44openalex-snapshot
On Thermodynamic Cycles for Detonation Engines
inferred← citeshttps://doi.org/10.1007/978-981-19-7927-9_1openalex-snapshot
Why Hypersonic Propulsion?
inferred← citeshttps://doi.org/10.1007/978-981-19-7927-9_4openalex-snapshot
Hypersonic Flight and Its Impact on Propulsion
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2023.121651openalex-snapshot
Influence of time-varying flow on dynamic flame characteristics in VCE: Numerical and experimental study
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2024.123709openalex-snapshot
A simplified numerical method based on anisotropic porous media model for the precooler of the hypersonic precooled engine
inferred← citeshttps://doi.org/10.1016/j.ast.2007.10.012openalex-snapshot
Propulsion vehicle integration for reusable launcher using in-flight oxygen collection
inferred← citeshttps://doi.org/10.1016/j.ast.2012.04.006openalex-snapshot
Highly cited literature of high-speed compressible flow research
inferred← citeshttps://doi.org/10.1016/j.ast.2015.12.026openalex-snapshot
Advantage of ethanol fuel for gas generator cycle air turbo ramjet engine
inferred← citeshttps://doi.org/10.1016/j.ast.2017.04.026openalex-snapshot
Experimental study of pyrolysis–combustion coupling in a regeneratively cooled combustor: System dynamics analysis
inferred← citeshttps://doi.org/10.1016/j.ast.2019.03.015openalex-snapshot
Performance modeling of pulse detonation engines using the method of characteristics
inferred← citeshttps://doi.org/10.1016/j.ast.2019.05.023openalex-snapshot
Alcohol and alkane fuel performance for Gas Generator cycle Air Turbo Ramjet Engine
inferred← citeshttps://doi.org/10.1016/j.ast.2021.106704openalex-snapshot
Robust design of an adaptive cycle engine performance under component performance uncertainty
inferred← citeshttps://doi.org/10.1016/j.ast.2022.107792openalex-snapshot
Acceleration technique for global optimization of a variable cycle engine
inferred← citeshttps://doi.org/10.1016/j.ast.2023.108579openalex-snapshot
A novel performance analysis framework for adaptive cycle engine variable geometry components based on topological sorting with rules
inferred← citeshttps://doi.org/10.1016/j.ast.2024.109284openalex-snapshot
A hybrid design method of steady-state throttling control schedules for high-flow variable cycle engine
inferred← citeshttps://doi.org/10.1016/j.energy.2025.134682openalex-snapshot
Matching mechanism of a novel variable cycle propulsion concept with hydrogen intercooling
inferred← citeshttps://doi.org/10.1016/j.jppr.2022.07.007openalex-snapshot
New insights into component matching mechanism in the compression system of double bypass engine
inferred← citeshttps://doi.org/10.1016/s0094-5765(99)00080-6openalex-snapshot
Benefits from incorporation of combined cycle propulsion
inferred← citeshttps://doi.org/10.1016/s0094-5765(99)00185-xopenalex-snapshot
Optimal supersonic intake design for air collection engines (ACE)
inferred← citeshttps://doi.org/10.1017/cbo9780511627019.005openalex-snapshot
Cycle Analyses and Energy Management
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0001492openalex-snapshot
Preliminary Study on Mixing Mechanism of Three-Dimensional Vortices in the Wake of Lobe-Type Rear Variable Area Bypass Injector
inferred← citeshttps://doi.org/10.1080/00102202.2014.965300openalex-snapshot
Development of a Liquid-Purge Method for High-Frequency Operation of Pulse Detonation Combustor
inferred← citeshttps://doi.org/10.1081/ss-120005473openalex-snapshot
DISTILLATION CASCADES BASED ON DIFFERENTIAL VAPORIZATION AND DIFFERENTIAL CONDENSATION STAGES. I. TWO-STAGE DCDV CASCADES
inferred← citeshttps://doi.org/10.1098/rsta.1999.0431openalex-snapshot
Topic II. Airbreathing propulsion
inferred← citeshttps://doi.org/10.1098/rsta.1999.0432openalex-snapshot
A demonstrator for the SSTO launcher with combined cycle propulsion
inferred← citeshttps://doi.org/10.1115/1.2372776openalex-snapshot
Effect of Blade Passage Surface Heat Extraction on Axial Compressor Performance
inferred← citeshttps://doi.org/10.15623/ijret.2016.0506050openalex-snapshot
EFFECT OF DIFFERENT NOZZLES ON THE PERFORMANCE OF PULSE DETONATION ENGINE- A REVIEW
inferred← citeshttps://doi.org/10.2298/tsci230403177wopenalex-snapshot
Numerical investigation on the heat transfer of air/helium precooler for air-breathing pre-cooled engine
inferred← citeshttps://doi.org/10.2514/1.10794openalex-snapshot
Effect of Rocket Exhaust Configurations on Ejector Performance in RBCC Engines
inferred← citeshttps://doi.org/10.2514/1.a36296openalex-snapshot
Hypersonic Point-to-Point Transportation Benchmark Study (Boost-Glide Versus Cruise): Methodology
inferred← citeshttps://doi.org/10.2514/1.b35446openalex-snapshot
Efficiency of an Ideal Brayton Cycle with a Constant-Volume Interturbine Burner
inferred← citeshttps://doi.org/10.2514/1.t7439openalex-snapshot
Real-Time Heat-Sink Capability Monitoring Framework of Fuel Thermal Management System
inferred← citeshttps://doi.org/10.2514/2.5305openalex-snapshot
Strategies for Pulsed Detonation Engine Performance Optimization
inferred← citeshttps://doi.org/10.2514/2.5563openalex-snapshot
Pulse Detonation Magnetohydrodynamic Power
inferred← citeshttps://doi.org/10.2514/2.6099openalex-snapshot
Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube
inferred← citeshttps://doi.org/10.2514/2.6166openalex-snapshot
System Performance and Thermodynamic Cycle Analysis of Airbreathing Pulse Detonation Engines
inferred← citeshttps://doi.org/10.2514/5.9781600866609.0757.0822openalex-snapshot
Liquid Hydrocarbon Fuels for Hypersonic Propulsion
inferred← citeshttps://doi.org/10.2514/6.1999-4830openalex-snapshot
LOX collection - A highly synergistic technology
inferred← citeshttps://doi.org/10.2514/6.2002-473openalex-snapshot
System performance and thermodynamic cycle analysis of air-breathing pulse detonation engines
inferred← citeshttps://doi.org/10.2514/6.2003-1168openalex-snapshot
Thrust Chamber Dynamics of Multi-Tube Pulse Detonation Engines
inferred← citeshttps://doi.org/10.2514/6.2003-4649openalex-snapshot
Effects of the Ascent Trajectory on the Operation and Performance of a TSTO ACES Propulsion System
inferred← citeshttps://doi.org/10.2514/6.2003-4890openalex-snapshot
Progress on ACES: Technology for Next Generation Space Transportation
inferred← citeshttps://doi.org/10.2514/6.2003-5037openalex-snapshot
Airport to Orbit, A Comparison of Horizontal Takeoff RLVs
inferred← citeshttps://doi.org/10.2514/6.2004-3310openalex-snapshot
Technology Demonstration of ATR with a Ramjet Test Facility
inferred← citeshttps://doi.org/10.2514/6.2009-5118openalex-snapshot
Current State of High Speed Propulsion: Gaps, Obstacles and Technological Challenges in Hypersonic Applications
inferred← citeshttps://doi.org/10.2514/6.2010-7169openalex-snapshot
System Design of a Reusable, Horizontal Take-Off/Horizontal Landing Two Stage to Orbit Vehicle
inferred← citeshttps://doi.org/10.2514/6.2017-4791openalex-snapshot
Steady-State Performance Comparison of Two Different Adaptive Cycle Engine Configurations
inferred← citeshttps://doi.org/10.2514/6.2018-4518openalex-snapshot
High-Level Power Extraction from Adaptive Cycle Engine for Directed Energy Weapon
inferred← citeshttps://doi.org/10.2514/6.2019-0172openalex-snapshot
Multipoint Variable Cycle Engine Design Using Gradient-Based Optimization
inferred← citeshttps://doi.org/10.2514/6.2020-2952openalex-snapshot
Exploratory Passive Control Study of a Supersonic Multi-Stream Nozzle Flow
inferred← citeshttps://doi.org/10.2514/6.2023-1464openalex-snapshot
Development of a Parametric Variable Cycle Engine Model Using the Multiple Design Point Approach
inferred← citeshttps://doi.org/10.2514/6.iac-03-s.5.03openalex-snapshot
ACES: Propulsion Technology for next Generation Space Transportation
inferred← citeshttps://doi.org/10.3390/aerospace10020112openalex-snapshot
Game-Theory-Based Mode Switch Control Schedule Design for Variable Cycle Engine
inferred← citeshttps://doi.org/10.3390/aerospace10020196openalex-snapshot
Variable-Geometry Rotating Components Modeling Based on Reference Characteristic Curves for the Variable Cycle Engine
inferred← citeshttps://doi.org/10.3390/aerospace12100882openalex-snapshot
Research on Quasi-One-Dimensional Ejector Model
inferred← citeshttps://doi.org/10.3390/aerospace9080431openalex-snapshot
Development and Validation of a Novel Control-Volume Model for the Injection Flow in a Variable Cycle Engine
inferred← citeshttps://doi.org/10.3390/en14123690openalex-snapshot
Some Key Issues in Hypersonic Propulsion
inferred← citeshttps://doi.org/10.5589/q05-013openalex-snapshot
Rocket Vehicle Design for Small-Payload Delivery to Orbit
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