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At mach 0.4 does the mirage-2000 have 18 deg turn rate?.
From Dr.Vivek Ahuja BRF
LCA vs Mirage 2000
Even F-16 A had just 17 deg turn rate at those velocities if my memory serves me right!!!! SO does mirage-2000 have a higher turn rate than F-16 A ?
Sir, Since you are SHIV in BR,I am no journo. I am only a foolish jingo like everyone else. But my handle is shiv, not shiv aroor and I have been around from when shiv aroor was still a twinkle in his father's eye. I would appreciate not being confused with shiv aroor or being thought of as a journo.
I am watching those posts Ahuja's in Br with interest.
Can you ask Ahuja to clarify on this single point ,
Can Mirage 2000 complete a vertical turn in 19 -20 seconds with 20 deg AOA limit and 6 G limit at an altitude 1000 plus meter above sea level at 30 plus degree atmospheric temp , like tejas mk1 did in aeroindia 2013? using the flight stream solver?
I really doubt it can do it, because even rafale completed that vertical loop in only with the same twenty odd seconds in Aeroindia 2013 in bangalore under the same condition.
Also the thrust vectoring and canard enabled Su-30 MKI takes the same twenty seconds to complete a vertical loop.
And in Aeroindia2013 or 2011 , I haven't seen typhoon, F-16 F-18 and Gripen completing the vertical loop in less than twenty seconds.
In case you have any info on that please post.
Also can his software accurately predict all the vortice effects of cranked delta wing on tejas? Because mirage-2000 has simple straight delta , tejas has a bit more complex wing with cranked double delta with a varying slopes for leading edge and conical camber
SO at altitude 15000 ft, fuel weight as the same percentage as that of mirage-2000 at mach 0.5 for the same conditions what is the STR of tejas mk1, above or below 14 deg?
ALso he once tried to explain his software to core CFD guys of ADA , and they were not interested because they have much higher competence in much more complex and accurate CFD models themselves.
because many test pilots including Suneeth krishna who had flown Mirage-2000 had rated tejas better than mirage-2000, but the graphs tell another story.
take offs in tejas are sharper than Mirage-2000 is the exact words I remember.
Also Late NTSE chief Riaz Khokar has clearly said that in many key respects LCA was better than mirage-2000 even in 2013, when Tejas hasn't crosses 20 deg AOA and 6Gs.
SO I dont think they cant be wrong.
Also regarding drag, most people use the old Cemilac report , which talks about WAVE drag "in the context of tejas mk1 failing to reach mach 1 in sea level conditions ".
But it has crossed the sea level supersonic speed in Goa hot weather trials in POWERLESS flutter test dive from 4 Kms to one Km , "while pulling out of the dive".
So how accurate is to use this argument for corner velocity (much lower than supersonic speeds) as the reason for lower Sustained turn rates ?
And ADA data points released for tejqas which Vivek Ahujha took were pertinent to indian atmospheric temp, which saps ten percent of engine thrust and twelve percent of wing lift compared to colder climates in which I assume Mirage-2000 data was released by Dassault, is my assumption.
this is Indranil's quote, has all that been factored into flight stream analysis of Vivek AhujhaDon't know. There are quite a few papers by Anand Kumar which shows that their simulations had good fidelity. In one paper, he did match results with the LCA wind tunnel test results. For some tests it was a perfect match. IIRC, the vortex breakdown reaches the TE at 33 degrees and the apex at 52 or 55 degrees. Not just that they got good results even with matching sharp edges and round edges with various radii. Similar results were published people at Jadavpur university. We know that some development did go on there
Bottom line: Range/Endurance and STR/ITR analysis are not decoupled. The aerodynamics binds both of them together for each aircraft. So an aircraft having very poor range on account of its aerodynamics is also going to have other effects visible in its maneuvering performance.
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These words of Vivek AHUJHA falls flat when we compare mig-29 Vs Mirage-2000!!!. SO certainly it cant be true
Because it is open knowledge that in terms of STR and ITR mig-29 beats mirage-2000 by miles even though difference in ranges or not that big..
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