Still putzing around with the flight dynamics so as to try to somewhat replicate the transonic "issues". As an early delta wing it was a great research project, but as with the X-3 suffered from being quite underpowered.
It's fairly easy to land with a few caveats; The Delta wing can be usefully taken to quite high AOA values, but with increasing induced drag. Landing approach is accomplished at about 10-11 deg AOA at about 145 knots, depending on weight. The min drag is at about 175-180 knots, so you are in the area of reverse command on approach, meaning increasing the AOA will soon result in greater drag and a steeper glide angle. The technique ids to stabilize the aircraft at the appropriate attitude/airspeed/AOA and keep it there, adjusting the glide path with thrust. Just realize that you will need to complete the roundabout/flare maneuver with enough energy to not make an airplane shaped hole in the runway.
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