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the so called soft limit of around 26 deg is the real usable combat alpha.
Anything beyond that the fighter behaves with as much aerodynamic efficiency as a kite and by the time it regains it's aerodynamic efficiency for its wings and regains its speeds it may be too late to survive in the merge.
Thats why American aviation experts always don't take Thrust vector enabled eye catching air show maneuvers as not of great combat significance.
the CEILMAC report talks about reduction of "SUPERSONIC WAVE DRAG" by going in for a fuselage plug.
This wave drags comes in only when Tejas cross the sound barrier not at other times.
Also it migt be entirely possible that the cross section between 4 and 5 meter length of fuselage may have been smoothened by other means in LSP-7 and 8 with out fuselage plug. But we don't have any details for it.
But simpletons take it as a subsonic ever present drag that stalls tejas. It is simply a wrong diagnosis.
people even forget that the under wing air intake of tejas always gets more air due to the huge wing area above it which chanels the air around into intake.The wing and air intake was specifically designed for that.
It is the upper wing which needs vortex based lift in high alpha for which cranked delta design is chosen. the lower wing and air intake will have no problem in any alpha.
Anything beyond that the fighter behaves with as much aerodynamic efficiency as a kite and by the time it regains it's aerodynamic efficiency for its wings and regains its speeds it may be too late to survive in the merge.
Thats why American aviation experts always don't take Thrust vector enabled eye catching air show maneuvers as not of great combat significance.
the CEILMAC report talks about reduction of "SUPERSONIC WAVE DRAG" by going in for a fuselage plug.
This wave drags comes in only when Tejas cross the sound barrier not at other times.
Also it migt be entirely possible that the cross section between 4 and 5 meter length of fuselage may have been smoothened by other means in LSP-7 and 8 with out fuselage plug. But we don't have any details for it.
But simpletons take it as a subsonic ever present drag that stalls tejas. It is simply a wrong diagnosis.
people even forget that the under wing air intake of tejas always gets more air due to the huge wing area above it which chanels the air around into intake.The wing and air intake was specifically designed for that.
It is the upper wing which needs vortex based lift in high alpha for which cranked delta design is chosen. the lower wing and air intake will have no problem in any alpha.