Moon
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No worries.
But also remember that a delta wing design will bleed more energy going into angular plane against the thrust axis. So every time you pitch your nose your airframe will have less energy.
that depends on how your initial planiform was optimized and the requirement of Wing loading, Now higher Wing loading also means that reaction force on wing surface, flexural strength requirements on the roots and the stress concentration (both static and dynamic) are way higher on the fuselage.
true
Not necessarily. Prime example is Mig29,Which can hit a higher AoA of limiter is overridden.
Here are few more aspects of Wing design.
http://faculty.dwc.edu/sadraey/Chapter 5. Wing Design.pdf
Here are a few threads on aircraft projects by @Manticore which you might find interesting
Combat Aircraft Projects & Designs - Index in 2nd post
Design characteristics of canard & non canard fighters
Is it true delta winged planes have a shorter combat radius?.