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shalav

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Viewing 15 posts - 91 through 105 (of 174 total)
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  • in reply to: AERO INDIA 2007 #2516212
    shalav
    Participant

    Robban,

    Ok!

    1. How does wing sweep effect turn rate?
    2. How does wing twist effect turn rate?
    3. How does turn rate not effect maneuverability and agility?

    I am looking for more than the simple “I think it does – so it must be true” answer you have been saying so far.

    If you don’t have anything other than your personal opinion, I will stick to the tried and tested formulas till something better comes along.

    Till then I do not think your opinion matters as much as the empirically derived formulas used by the entire industry.

    I’ll be back tomorrow to read, and hopefully learn something from you.

    in reply to: AERO INDIA 2007 #2516226
    shalav
    Participant

    Gripen is unlikely to need it as the RM12 already use a larger fan than the F404.

    err, the F404/RM12 has the SAME fan dia. as the F404/F2J3 from which the F404/IN20 has evolved. What are you going on about?

    Here are the specifications of both from http://www.geae.com/engines/military/comparison_turbofan.html

    RM12 ::: F2J3

    Fan/Compressor Stages: 3/7 ::: 3/7
    Low-Pressure Turbine / High-Pressure Turbine: 1/1 ::: 1/1
    Maximum Diameter (Inches): 35 ::: 35
    Length (Inches): 154 ::: 154
    Dry Weight (Lb.): 2,325 ::: 2335

    Power Specifications
    Specific Fuel Consumption at Maximum Power: 1.78 ::: 1.8
    Max. Power at Sea Level: 18,100 ::: 18,300
    Overall Pressure Ratio at Maximum Power: 27 ::: 27

    in reply to: AERO INDIA 2007 #2516239
    shalav
    Participant

    Robban,

    There is a way to calculate these figures. Given the same conditions of altitude, fuel and armament, the Tejas exhibits better ITR performance, and this can be shown to be mathematically true.

    mainly because of:-

    a) lower corner velocity – which is actually derived from its lower weight

    b) lower wing loading because of
    i. greater wing area of the Tejas:Gripen – 38 m2:31.08 m2 including canard area
    ii. lower empty weight of the Tejas:Gripen – 5,500 kg:6,620 kg

    You have an opinion as to how much better the canarded Gripen is as compared to the compound delta of the Tejas, I feel differently. I will leave it at that, I am not really concerned about opinion, only what can be shown empirically.

    While the Gripen has been rumoured to be an MRCA contender, it really does not belong in the league, as far as the IAF is concerned.

    It really should be competing with the Tejas in the LCA role, rather than an MCA role for the IAF. Both have similar performance more or less. However in such a competition it would probably loose out to the Tejas, because of the price factor. The IAF could probably purchase between 1-2 Tejas’ for every Gripen.

    in reply to: AERO INDIA 2007 #2516317
    shalav
    Participant

    Robban,

    Here are some reasons how instantaneous turn rate is affected.

    1. Velocity
    2. Weight
    3. Wing loading
    4. Altitude

    The lower the velocity the faster the turn rate. This is observable even when one drives ones car. The slower it is the quicker it will turn.

    Wing loading effects how quickly the aircraft can turn.

    Weight effects corner velocity.

    Altitude = air density and air pressure, which in turn effect the lift:drag ratio, which in turn effect corner velocity, which directly effects Instantaneous Turn Rate (ITR).

    Corner velocity is the minimum velocity at which the maximum g rate can be attained. This is when the aircraft is the most manoeuvreable.

    Anyone who makes a statement about turn rates should also be able to state the conditions under which such a manoeuvre is being observed. Further if you want to compare 2 airframes then you should be able to state that the results are based on similar conditions. As conditions change so will the observed results.

    Most times, people forget to evaluate the conditions under which such comparisons are made. Such comparisons are a waste of time.

    This is the reason I put together an excel worksheet. BTW I am not an expert, simply someone who put together formulas which are available in the public domain in one convenient worksheet.

    If you want to compare the Gripen and the Tejas, I am willing to listen to your figures and debate them mathematically. But if you do not want to be dismissed as someone simply repeating marketing blurbs you should state conditions under which such results were observed. Without this your statements about turn rates hold no water.

    In the meantime I stand by what Joey wrote up-thread, except to add the turn rates quoted are ITR and not sustained turn rates (relevant corner velocities as also other conditions are also provided in the same quote).

    in reply to: Why all MiG #'s odd? #2532225
    shalav
    Participant

    I think their transports and bombers are even numbered, fighters and strike aircraft have odd numbers – mostly.

    Notable execption would be the Su30 derivative of the Su27!

    in reply to: SU-33 take off without catapult? #2587946
    shalav
    Participant

    Kilocoo316,

    Assuming the rotation performed by the ski jump is the only effect is a fundamental error. While it does perform a rotation – unlike in normal non-ski-jump-assited takeoffs – ground effect performance is not decreased. Hence it does a lot more than only induce rotation or impart ‘vertical speed’. It increases lift efficiency AND maintains the same low drag due to ground effect.

    This is no small matter, drag reduction due to ground effect has been calculated to be about half as without ground effects. IOW during a normal takeoff the moment a rotation is performed drag effects double, a ski ramp maintains this low drag effect alongwith the increase in lift.

    in reply to: SU-33 take off without catapult? #2588293
    shalav
    Participant

    Kilocoo316,

    1. Your calculations for takeoff distance do not include WIG. Without factoring in WIG, you cannot calculate takeoff distance which is reasonably close t0 the actual distance.

    2. The ski ramp is not supposed to induce ‘vertical speed’. The ski ramp changes the angle of attack. This forces greater lift along with the reduced drag due to WIG, which in turn means lower V for VR with a lower drag due to WIG still being a factor till the point the aircraft actually exits the ski ramp.

    3. Many other factors (runway friction, air density, air temprature, altitude – actually in this case you should consider ISA sea level standards for density, temprature and altitude, flap position and its effect on CD0, Wing aspect ratio -without which you cannot calculate CL, max) are not considered in that equation.

    A good aproximation of takeoff distance can be arrived at by using:

    SLO = (1.44 W2) / [g ρ S CL,max {T – [D + μr (W – L)]}]

    μr = Friction from runway – Use these values generally accepted values

    .-.Dry concrete/Asphalt – 0.02
    .-.Long grass – 0.10
    .-.Hard turf/Gravel – 0.04 (approximation of aircraft carrier deck)
    .-.Soft Ground – 0.10 to 0.30
    .-.Short, dry grass – 0.05

    D = Drag; and for rolling takeoff you will use this formula

    D = 0.5 ρ V2 S [CD0 + (φ CL2) / (π A e)]

    ρ = Air Density (for sea level use 1.2250 kg/m3)
    V = velocity
    S = Wing Area
    CD0 = Zero Lift Drag co-efficient
    A = Aspect ratio (Square of the wingspan / wing area)
    e = Oswald Efficiency
    φ = Drag reduction due to ground effect – this is calculated as:

    φ = [16h/b]2 / [1 + (16h/b)2]

    h = height of the wings
    b = wing span

    Normally I would not interfere, since other conclusions are being based on only these calculations, we should have the right numbers to conclude anything derived from these works.

    You should also look at this paper for more info on take off and landing formulas

    http://atlas.cc.itu.edu.tr/~acarh/flight-mech/flight-m-6.pdf

    in reply to: Kuznetsov vs Vikramaditya #2057719
    shalav
    Participant

    No offence taken. But I feel I must point out some things which you have missed in my post, and have repeated again.

    1. The last statement I made was “Thats my opinion – take it FWIW.” You are free to express your own opinion as you see it.

    2. Experience gained is never lost. That is a fundamental misconcpetion. A deck crew chief has spent his life on the carrier, there is no other place for him to go. His eventual replacement started as a deck hand and will replace him. Along the way he has absorbed the crew chiefs knowledge and added some more of his own. He will pass this to his successor and so on. Thats how experience is passed on in real life. The navy is already training the next crew chief once a new one is appointed. I fail to see how this continuity of experience can ever be lost? This is the case with officers too. It would be foolish for any navy to wait for a crew member to retire before training his/her replacement.

    Furthermore on the one hand while you accept there is an knowledge gap which may take ~3-10 years to cover (which is what I said more or less), but on the other you say “Knowledge is recorded in manuals, and manuals can be bought”, thereby implying such knowledge can be gained and instantly applied to carrier operations by talking to others, instead of gaining it for oneself.

    …Crews come and go with time, and experience is lost with the men, knowledge is not. Knowledge is recorded in manuals, and manuals can be bought…

    To sum up, just because the PLAN have not operated carriers before does not mean that they can’t learn from others instead of trying everything in-house and doing everything the hard way. And any operational experience gap between the two sides would disappear pretty quick once a carrier is in operation. So any noteworthy difference in crew quality between the PLAN and IN in terms of carrier ops will only last for a fairly short period of 3~10 years.

    I’m really not sure what the thrust of your debate is? If you have already conceeded to the gap and agree that it may take ~3-10 years to catch up, aren’t you more or less in agreement with my post?

    As regards proponents of the IN, I really don’t take this as a mine is bigger than yours. Its my opinion – feel free to disagree.

    in reply to: Kuznetsov vs Vikramaditya #2057741
    shalav
    Participant

    RE: Operating experience on carriers:

    I would liken it to riding a motorcycle as an analogy. Let me explain

    Some motorcycle experiences are common to the whole event and can be applied across all models, and some experiences can only be gained by riding the particular model.

    Common experiences which can be applied across all models such as:-

    – Is the dark patch I see up the road a pothole, water, oil or just a simply a shadow?

    When one is new to the motorcycle experience one tends not to notice such things till one of these actually causes one to have an accident or a near accident. The motorcycle riding experience forces one to see the road differently than if one is riding a car. After ones first spill or near accident one tends to be more cautious, and avoid all the dark patches. Sometime later as one gains experience handling the motorcycle and there is a general increase in ones confidence, one will evaluate everything including the surrounding environment and act accordingly. At that time handling the dark patches on the road will be done almost automatically as they occur. One will ride faster and cut corners when neccessary because one knows what ones machine and one can handle. Where the machines breaking points are, and how hard one can push oneself.

    Experiences which can be gained by only by riding a particular model such as:-

    – How are the gears arranged? How tight is the clutch? What is the braking distance, and how quickly can the machine come to rest? Does the machine drift to the left or right when applying emergency brakes? How far can I push it on reserve fuel? How comfortable are the seats? What is the best riding position for this machine? What is the redline? What is needed to carry out on-the-go repairs to get me home?

    For someone who has ridden all types of motorcycle for 50 years, it is easier to adapt to a new machine because that someone can call on previous experience. A newbie has to adapt to both the machine and the road (environment) simultaneously. Hence you will always find a newbie will be slower and less agile than the experienced motorcycle rider.

    Similarly when operating a carrier, the IN has more “road experience” with varied machines. They can apply such “road experiences” to newer types of carriers on-the-go. For instance:-

    Do these particular sea conditions mean it can launch and recover its aircraft safely and in a timely manner? Are the local conditions advantageous to avoid a fight or seek it? These are examples of environmentally influenced common experiences.

    What is the surge sortie rate? How much stores are sufficient for this particular engagement? What maintainence can get me home in one piece? What can be deferred till we make port? These are experiences gained from the use of a particular machine. Again more quickly gained because of previous experience.

    The IN has operated STOVL and CATOBAR carriers for almost 50 years. Such experience is not lost, some of those experiences may be a little rusted, but its not lost. Specially the environment experiences, these are never lost, as they are passed on and added to from generation to generation. STOBAR operations are different, but not an out-of-the-box experience for the IN. They’ll find it easier to adapt quickly to operating STOBAR carriers.

    I’m not saying the PLAN will never gain the experience, just that it’ll be some time before they are as agile or speedy as the IN as far as carrier ops are concerned, thats all.

    The PLAN is switching from riding cars to riding motorcyles, the IN has been riding motorcycles for the past 50 years. Just as you’d expect an experienced rider to win the Isle of Man TT over a newbie riding a motorcycle in that event for the first time, similarly you’d expect an IN CVBG to prevail over a PLAN CVBG – at-least for the next 5-10 years. Thats my opinion – take it FWIW.

    shalav
    Participant

    …Shalav..I dont care that Agni is of Stealth/MRV capable..india should go on..and more..they will hurt themselves..Like Pakistan..because nobody is going to use it…same is with Iran ar such crucial stage ..they are testing missiles all the war mongring…by both sides..

    I don’t care either! I thought your statement about it “resembling an Agni” meant you had some insights. Apparently its just hot air. So lets just stick to talk about the Iranian missile.

    shalav
    Participant

    I just it on TV..the missiles resembles like agni SSM..

    Cool – Does that mean the Agni is also a stealth / MIRV capable missile? 😀

    in reply to: F-15N Sea Eagle #2587830
    shalav
    Participant

    Thats a nice conception. The only (minor) thing that spoils it for me is the absence of the recognizeable raked wingtips of the ‘normal’ F15.

    in reply to: Faked apollo Mission to Moon? #2588020
    shalav
    Participant

    Debunk:

    General

    http://www.iangoddard.net/moon01.htm – very good

    http://www.straightdope.com/mailbag/mmoonhoax.html

    http://www.braeunig.us/space/hoax.htm

    http://www.thekeyboard.org.uk/Did%20we%20land%20on%20the%20Moon.htm

    http://www.redzero.demon.co.uk/moonhoax/

    http://www.badastronomy.com/bad/tv/foxapollo.html – Check out his entire website. Its really really good – http://www.badastronomy.com/

    Van Allen Belt

    http://spider.ipac.caltech.edu/staff/waw/mad/mad19.html

    http://www.madsci.org/posts/archives/may2000/959341359.As.r.html

    If you are still not convinced – click here to satiate your conspiracy theories.

    Or this even more odd ones

    http://www.lunaranomalies.com/czarnik.htm

    If you really want conspiracy theories see

    http://www.enterprisemission.com/

    Hoagland does not limit himself to only the moon. Time to bring out the tinfoil! :dev2:

    in reply to: fuji 9500 v olympus e500 v nikon d50 v canon eos 350d #464531
    shalav
    Participant

    Here’s what I think.

    If you forsee any limitation with the Fuji lens then go for a SLR. The money you will spend on getting accessory lenses for the Fuji would be better spent on getting lenses for the SLR you choose.

    Sensor size:
    This means the physical dimensions of the sensor (not the megapixels crammed within the lenght and breadth of that sensor). This is the most overlooked aspect when purchasing a digital camera. The size of the sensor will affect the quality of the image. As a thumb rule, the larger the sensor size the better image quality. This is because larger sensors enable the manufacturer to use larger individual sensors, which means those are more sensitive to light than smaller sensors. Hence better quality of the image. In increasing order of sensor size

    Fuji Fuji
    Olympus E500
    Canon D350
    Nikon D50

    Lens compatibility:
    If you go for an SLR, you will eventually feel the need for a different lens than from the kit one you got with the camera. The ability to use different lenses for different situations is what makes SLRs so popular. The big daddy of backward lens compatibility are the Nikons and Pentax’s. You can use lens released 40 years ago with their modern DSLRs even today. Of-course no auto features, but you can find cheap old compatible lenses for them. Canon really muffed it when they changed their lens system from the old FD to EF. They had their reasons, but as an owner of a set of (expensive) FD lenses for my AE1 it really bothered me. However their EF and EF-L lenses are pretty good glass. Olympus opted for a 4/3rd sensor size for their digital offerings. AFAIK their Zuiko series are more expensive than comparable Canon or Nikon glass. Further no other 3rd party manufactuer offers cheaper alternatives for their zuiko lenses. For Nikon or Canon you can purchase cheaper glass from manufacturers such as Tamron, Sigma, Tokina etc…

    Image processing engine:
    The image processing engine which comes with the camera can vary a lot. You should compare images of similar shots taken under similar conditions at sites such as Dpreview.com

    Lastly, but the most important. Your budget.

    Final note:
    You don’t have to be an equipment measuretubator. If a pinhole camera can give you what you want, you dont need to spend large amounts of money to get the latest and greatest SLR or digicam. Decide what you want to do with the camera. Research the capabilities of the ones you shortlist and go for it. I’m sure you will enjoy hundreds of hours pleasureable photography.

    As for me – after my AE1 I used a kodak P&S for 15 years before I decided I wanted to get back to SLR photography, so I went out and bought the Canon 350D. It gives me most of what I am looking for. I didn’t need obscenely fast picture taking 2.7 FPS for upto 14 images was good enough for me. It can use EF, EF-S and EF-L lenses. The thing that decided it for me was the availability of an FD to EF converter. That meant I could use my old FD lenses. If not for that it would have been a difficult choice between the D50 and D350 for me personally.

    in reply to: fuji 9500 v olympus e500 v nikon d50 v canon eos 350d #464533
    shalav
    Participant

    Try this side-by-side comparison

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