What is the stall speed and AOA of an f-14 with wings fully swept back?

For an F-14 Tomcat with its wings fully swept back, several key points can be noted, although the exact stall speed and angle of attack (AOA) are not explicitly provided in the sources:

Stall Speed

When the F-14's wings are fully swept back to 68 degrees, the aircraft experiences a significant increase in stall speed. This is because the swept-back configuration reduces the effective wingspan and increases the wing loading, leading to a higher stall speed. While the exact stall speed is not specified, it is mentioned that landing with the wings fully swept back presents a significant safety hazard due to the greatly increased stall speed35.

Angle of Attack (AOA)

The angle of attack at which the wing stalls is generally influenced by the wing's aspect ratio and the presence of high-lift devices. For a swept wing configuration, the stall tends to occur at a higher angle of attack compared to a high aspect ratio wing. However, the specific AOA for an F-14 with fully swept-back wings is not provided in the sources.

In general, swept wings tend to stall at higher angles of attack, but the exact AOA for the F-14 in this configuration would require specific aerodynamic data or test results, which are not detailed in the available sources14.

In summary, while the exact stall speed and AOA for an F-14 Tomcat with fully swept-back wings are not provided, it is clear that the stall speed increases significantly, and the AOA at stall would be higher than that of a high aspect ratio wing.