Experimental Tests and Numerical Analysis of Aerodynamic Properties of the Composite-Made Jet-Propelled Aerial Target. [PDF]
Frant M+3 more
europepmc +1 more source
A DLSTM-Network-Based Approach for Mechanical Remaining Useful Life Prediction. [PDF]
Liu Y+5 more
europepmc +1 more source
Environmental and High-Strain Rate effects on composites for engine applications [PDF]
The Lewis Research Center is conducting a series of programs intended to investigate and develop the application of composite materials to structural components for turbojet engines.
Chamis, C. C., Smith, G. T.
core +1 more source
DESIGN AND DEVELOPMENT OF A 70 N THRUST CLASS TURBOJET ENGINE
P. E. Trazzi
openalex +2 more sources
Evaluation of methods for characterizing the fine particulate matter emissions from aircraft and other diffusion flame combustion aerosol sources. [PDF]
Giannelli R+22 more
europepmc +1 more source
Summary of investigations of engine response to distorted inlet conditions [PDF]
A survey is presented of experimental and analytical experience of the NASA Lewis Research Center in engine response to inlet temperature and pressure distortions.
Abdelwahab, M.+3 more
core +1 more source
Characterizing and Predicting nvPM Size Distributions for Aviation Emission Inventories and Environmental Impact. [PDF]
Durdina L+9 more
europepmc +1 more source
Metal 3D printing as a disruptive technology for superalloys. [PDF]
Panwisawas C, Tang YT, Reed RC.
europepmc +1 more source
Preliminary engineering report for design of a subscale ejector/diffuser system for high expansion ratio space engine testing [PDF]
The design of a subscale jet engine driven ejector/diffuser system is examined. Analytical results and preliminary design drawings and plans are included. Previously developed performance prediction techniques are verified. A safety analysis is performed
Doktor, M. F.+2 more
core +1 more source