Pages that link to "Item:Q1388008"
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The following pages link to Numerical solution for complete aircraft's subsonic-transonic-supersonic flow at high angles of attack (Q1388008):
Displaying 3 items.
- Numerical modeling of supersonic flow over wings with varying aspect ratio on a broad range of angles of attack using the law of plane sections (Q1317696) (← links)
- Numerical solution for complete aircraft's subsonic-transonic-supersonic flow at high angles of attack (Q1388008) (← links)
- Approximate solutions of range for constant altitude – constant high subsonic speed flight of transport aircraft (Q5706528) (← links)