Pages that link to "Item:Q3061467"
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The following pages link to Details on the Computation of Hypersonic Inlet Flows (Q3061467):
Displaying 6 items.
- An improved method to determine free stream conditions in hypersonic facilities (Q1312605) (← links)
- Distinctive features of the lateral flow for a convergent air-intake with a convergent nose compression surface (Q1403647) (← links)
- A new concept and preliminary study of variable hypersonic inlet with fixed geometry based on shockwave control (Q2468314) (← links)
- Three-dimensional flow simulations for supersonic mixed-compression inlets at incidence (Q3216332) (← links)
- Hypersonic aircraft and inlet configurations derived from axisymmetric flowfields (Q3359925) (← links)
- (Q5268544) (← links)