Ferlauto et al., 2018 - Google Patents
Computational investigation of injection effects on shock vector control performanceFerlauto et al., 2018
- Document ID
- 3558272812784861922
- Author
- Ferlauto M
- Marsilio R
- Publication year
- Publication venue
- 2018 Joint Propulsion Conference
External Links
Snippet
Designing and developing new aerospace propulsion systems is time-consuming and expensive. Computational simulation is a promising means for alleviating this, due to the flexibility it provides for rapid and relatively inexpensive evaluation of alternative designs …
- 230000035939 shock 0 title description 22
Classifications
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- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
- G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
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- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F2217/00—Indexing scheme relating to computer aided design [CAD]
- G06F2217/16—Numerical modeling
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