Effect of nose bluntness Intake Features on Hypersonic Inlet Flow Field by V.B.
29,17 €
The effect of nose bluntness intake features on hypersonic inlet flow field is an important area of research for the design and optimization of hypersonic aircraft. The nose bluntness of the intake features can affect the flow field characteristics, which can in turn impact the performance of the engine and the aircraft as a whole.The research on the effect of nose bluntness intake features on hypersonic inlet flow field involves the use of computational fluid dynamics (CFD) simulations to study the flow characteristics of the inlet features.
Jetzt bei Ebay:
![Produktbild - Loading tests of a wing structure for a hypersonic aircraft / Ro [Leather Bound]](https://i.ebayimg.com/thumbs/images/g/EZkAAOSwSC5nh2S6/s-l140.jpg)
