Preparation, Mechanical Properties and Strengthening Mechanism of W-Re Alloys: A Review. [PDF]
Materials (Basel), 2023 Zheng Z +5 more
europepmc +1 more source
Development of high temperature materials for solid propellant rocket nozzle applications [PDF]
Aspects of the development and characteristics of thermal shock resistant hafnia ceramic material for use in solid propellant rocket nozzles are presented.
Lineback, L. D., Manning, C. R., Jr.
core +1 more source
Computer code for the prediction of nozzle admittance [PDF]
A procedure which can accurately characterize injector designs for large thrust (0.5 to 1.5 million pounds), high pressure (500 to 3000 psia) LOX/hydrocarbon engines is currently under development.
Nguyen, Thong V.
core +1 more source
A generalized method for the design of optimum rocket nozzles
, 1967 Harvey Leo Rozendaal
openalex +1 more source
Apparatus for changing the orientation and velocity of a spinning body traversing a path Patent [PDF]
, 1968 Development of method and apparatus for spinning satellite about selected axis after reaching predetermined ...
Rosen, H. A., Williams, D. D.
core +1 more source
Flow Separation Side Loads Excitation of Rocket Nozzle FEM [PDF]
, 2007 Kurt Smalley +3 more
openalex +1 more source
Performance of rocket nozzle materials with several solid propellants [PDF]
Erosion resistance and thermal stress cracking tests of rocket nozzle materials with solid ...
Freche, J. C. +2 more
core +1 more source
Aerodynamic spike nozzle Patent [PDF]
, 1966 Constructing fluid spike nozzle to eliminate heat transfer and high temperature problems inherent in physical ...
Cowell, T. E., Madison, I. B.
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Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle
, 1987 Kenneth J. Kacynski +2 more
openalex +2 more sources
Computational design exploration of rocket nozzle using deep reinforcement learning
Results in EngineeringDeep Reinforcement Learning (DRL) has emerged as a powerful tool for solving high-dimensional optimization problems in complex, unexplored domains. This study presents a novel application of DRL for computational design exploration of rocket nozzles ...
Aagashram Neelakandan +2 more
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