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Thermodynamic Analysis for a Novel Chemical Precooling Turbojet Engine Based on a Multi-Stage Precooling-Compression Cycle

https://doi.org/10.2139/ssrn.4102737
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15/15 checkable references clean · checked 2026-08-28

Every reference with a DOI in the deposited reference list resolved to a known work in Crossref or DataCite at the dated check, and none carried a retraction, withdrawal, or removal notice.

32 without a DOI — not checked. A reference deposited without a DOI is never matched by title or guessed at; it stays outside the checked set, and this line discloses that.

The 15 checked references that resolve
resolves10.1016/j.actaastro.2018.09.002
An overview of waverider design concept in airframe/inlet integration methodology for air-breathing hypersonic vehicles
resolves10.1016/j.enconman.2018.03.058
Experimental and theoretical investigation of power generation scheme driven by thermal cracked gaseous hydrocarbon fuel for hypersonic vehicle
resolves10.1016/j.energy.2015.08.017
Thermodynamic analysis on optimum performance of scramjet engine at high Mach numbers
resolves10.1016/j.actaastro.2020.07.039
Key technologies for thermodynamic cycle of precooled engines: A review
resolves10.1016/j.cja.2020.03.028
Micromanufacturing technologies of compact heat exchangers for hypersonic precooled airbreathing propulsion: A review
resolves10.2514/6.1999-4897
Development study on precooler for ATREX engine
resolves10.1016/j.enconman.2019.06.049
Thermodynamic analysis of the influential mechanism of fuel properties on the performance of an indirect precooled hypersonic airbreathing engine and vehicle
resolves10.1016/j.actaastro.2017.06.011
Thermodynamic efficiency analysis and cycle optimization of deeply precooled combined cycle engine in the air-breathing mode
resolves10.1016/j.ijhydene.2019.02.133
Assessment of NOx emissions of the Scimitar engine at Mach 5 based on a thermodynamic cycle analysis
resolves10.1016/j.enconman.2018.03.088
Hydrogen production, storage, transportation and key challenges with applications: A review
resolves10.1016/j.rser.2015.05.011
Hydrogen storage: Materials, methods and perspectives
resolves10.1016/j.enconman.2009.04.023
Performance limit analysis of Recooled Cycle for regenerative cooling systems
resolves10.1016/j.ijhydene.2009.06.006
Parametric performance analysis of multiple Re-Cooled Cycle for hydrogen fueled scramjet
resolves10.2514/1.B34781
Modeling, Analysis, and Optimization of theAir-Turborocket Expander Engine
resolves10.1016/j.actaastro.2021.12.050
A hydrogen peroxide electric pump for throttleable hybrid rocket motor
The 32 references without a DOI — listed, not checked
no DOI — not checkedref3
no DOI — not checkedLAPCAT II: conceptual design of a Mach 8 TBCC civil aircraft, enforced by full Navier-Stokes 3D nose-to-tail computation
no DOI — not checkedHigh-elevation equatorial catapult-launched RBCC SSTO spaceplane for economic manned access to LEO
no DOI — not checkedref7
no DOI — not checkedref8
no DOI — not checkedref9
no DOI — not checkedref11
no DOI — not checkedA concept of LACE for SSTO space plane
no DOI — not checkedDesign Study on a Small Pre-Cooled Turbojet Engine for Flight Experiments
no DOI — not checkedref16
no DOI — not checkedref17
no DOI — not checkedref18
no DOI — not checkedPrinciples and realizing ways of combined power system for pre-cooling air turbo rocket
no DOI — not checkedThe sensitivity of precooled air-breathing engine performance to heat exchanger design parameters
no DOI — not checkedSustained Hypersonic Flight in Europe: Technology Drivers for LAPCAT II
no DOI — not checkedConfiguration optimization of the tandem cooling-compression system for a novel precooled hypersonic airbreathing engine
no DOI — not checkedThermodynamic design and optimization of the multi-branch closed Brayton cycle based precooling-compression system for a novel hypersonic aeroengine
no DOI — not checkedref27
no DOI — not checkedThermodynamic analysis of chemical precooled turbine combined engine cycle
no DOI — not checkedref33
no DOI — not checkedEmpirical expressions for estimating length and weight of axial-flow components of VTOL powerplants
no DOI — not checkedThermodynamic Analysis for a Novel Steam Rankine Cycle Based Indirect Chemical Precooled Engine Used for Supersonic Flight
no DOI — not checkedPure and Pseudo-pure Fluid Thermophysical Property Evaluation and the Open-Source Thermophysical Property Library CoolProp
no DOI — not checkedref37
no DOI — not checkedref39
no DOI — not checkedref40
no DOI — not checkedref41
no DOI — not checkedref44
no DOI — not checkedref45
no DOI — not checkedref46
no DOI — not checkedref47
no DOI — not checkedref48
What this badge says. CiteStamped means the CHECKABLE references of this work were clean at the dated check: each resolved to a known work in a public registry, and none carried a retraction notice at that time. If Crossref’s record marks the work itself retracted, withdrawn, or removed, the badge says so instead of showing clean. It says nothing about the quality, findings, or importance of the work itself, and nothing about references deposited without a DOI.

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