Data regarding dynamic performance predictions of an aeroengine. [PDF]
Data Brief, 2020 De Giorgi MG, Quarta M.
europepmc +1 more source
Large-Eddy Simulation on the Aerodynamic and Thermal Characteristics in a Micropipe of the Hypersonic Engine Precooler. [PDF]
Micromachines (Basel), 2022 Zhang J, Zou Z, Wang Y.
europepmc +1 more source
Durability of zirconia thermal-barrier ceramic coatings on air-cooled turbine blades in cyclic jet engine operation [PDF]
Thermal barrier ceramic coatings of stabilized zirconia over a bond coat of Ni Cr Al Y were tested for durability on air cooled turbine rotor blades in a research turbojet engine.
Jacobs, R. E. +3 more
core +1 more source
Effect of Chevron Nozzles on Turbojet Engine Performance and Jet Noise
, 2017 Gakuyo Tamada +2 more
openalex +1 more source
Study on Microwave-Assisted Ignition Using a Novel Aero-Engine Combustor. [PDF]
Sensors (Basel), 2023 Zhang Y, Zhao B, He L, Zeng H, Chang Y.
europepmc +1 more source
Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine. 7: Rotor-Blade Fabrication Procedures [PDF]
An experimental investigation was conducted to determine the cooling effectiveness of a wide variety of air-cooled turbine-blade configurations. The blades, which were tested in the turbine of a - commercial turbojet engine that was modified for this ...
Esgar, Jack B., Long, Roger A.
core +1 more source
An Experimental Investigation to Use the Biodiesel Resulting from Recycled Sunflower Oil, and Sunflower Oil with Palm Oil as Fuels for Aviation Turbo-Engines. [PDF]
Int J Environ Res Public Health, 2021 Cican G +4 more
europepmc +1 more source
Investigation of Combustion of the Gas Turbine Engine from Kerosene and Biokerosene and Their Soot Characteristics in Diffusion Flames. [PDF]
ACS Omega, 2022 Hong TD +3 more
europepmc +1 more source
The design and performance estimates for the propulsion module for the booster of a TSTO vehicle [PDF]
A NASA study of the propulsion systems for possible low-risk replacements for the Space Shuttle is presented. Results of preliminary studies to define the USAF two-stage-to-orbit (TSTO) concept to deliver 10,000 pounds to low polar orbit are described ...
Maldonado, Jaime J. +1 more
core +1 more source
Design Optimization of a Gas Turbine Engine for Marine Applications: Off-Design Performance and Control System Considerations. [PDF]
Entropy (Basel), 2022 Machmudah A +6 more
europepmc +1 more source