Equations and charts have been presented for the conical part of the sidewash above and below swept wings at small angles of attack. This flow-field component is necessary in making calculations of the wing-induced forces and moments on stores, missiles, and pylons. All supersonic Mach numbers and wing leading-edge sweep angles have been considered.
Sidewash in the Vicinity of Lifting Swept Wings at Supersonic Speeds
1957-02-01
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1956
|Downwash and sidewash fields behind cruciform wings
NTRS | 1952
|