114
P. Liu
Fig. 2.48 Flow around bat
Fig. 2.49 Wake vortex downwash
speed dial at any time. When the ground speed is reached, the pilot can pull
the rod to take off.
For tactical missiles and supersonic fighters, in order to reduce the wave
drag of flight performance, a small aspect ratio wing (aspect ratio less than
3) is usually used, and a sharp edge, non-bending, torsional, symmetric,
and large swept delta thin wing is usually used for the wing (as shown in
Fig. 2.52). For the flow around a swept delta wing with a small aspect ratio
P. Liu
Fig. 2.48 Flow around bat
Fig. 2.49 Wake vortex downwash
speed dial at any time. When the ground speed is reached, the pilot can pull
the rod to take off.
For tactical missiles and supersonic fighters, in order to reduce the wave
drag of flight performance, a small aspect ratio wing (aspect ratio less than
3) is usually used, and a sharp edge, non-bending, torsional, symmetric,
and large swept delta thin wing is usually used for the wing (as shown in
Fig. 2.52). For the flow around a swept delta wing with a small aspect ratio