dark light

Schorsch

Forum Replies Created

Viewing 15 posts - 3,451 through 3,465 (of 3,480 total)
  • Author
    Posts
  • in reply to: RA-5 Vigilante, your thoughts… #2067761
    Schorsch
    Participant

    It is often written that the MiG-25 Foxbat was built to counter the B-70 Valkyrie, and was put into production out of some kind of inertia after the bomber was cancelled. I think the continued existance of the RA-5C had a lot to do with it.

    The RA-5 was never a threat. It was a reconaissance aircraft. What should it have to do with the MiG-25?
    As I said that are only rumours and nobody can say if they are true.

    in reply to: RA-5 Vigilante, your thoughts… #2067774
    Schorsch
    Participant

    The Vigilante was ahead of its time. However, this comes with a price and that price is high and measured in Dollars. Problematic was like all designs of that time the high maintenace costs and low availability. It had the mission fading away but excelled as reconaissance aircraft. Actually NA re-opened the factory line to build new RA-5 in the Vietnam war.

    It would have been a reasonable platform for a land-based strike aircraft and even as interceptor. The focus on supersonic weapons delivery was typical for its time.

    There are rumours that the Russians were so impressed by the Vigilante at the 1959 Paris Air Show, that the used its general arrangement as starting point for the MiG-25.
    The arrangement of the Vigilante was unique at its time with new intake technology. It nearly got a second fin because directional stability seemd to be a problem (as it was with the MiG-25).

    in reply to: VLA sensitivity to wakes #588904
    Schorsch
    Participant

    Hm, that is strange. The ICAO recommended wake separations are 4 miles for a Heavy behind Heavy on approach/take-off, 5 miles for cruise – only 25 % bigger. For a Heavy behind Ai-380, it is 10 miles for approach/take-off, 15 miles for cruise – only 50 % bigger. Whereas the cruise speed, at about 0,85 Mach or 500 knots TAS, is at least 200 % greater than the speeds on approach/take-off (around 150 knots…). So a plane at a minimum safe distance behind a craft cruising ahead is leaving at most a half, and likely one-third, the time for wake decay that is allowed on approach/take-off.

    How do the separation requirements change from 4 miles takeoff limit to 5 miles cruise limit over the course of the climb?

    And that is reasonable, because wake intensity is not constant. It decreases with airspeed and configuration, so that the wake of a cruising aircraft is considerably lower amplitude than that of a approaching aircraft with similar weight. Same with sensitivity: At cruise speed a wake would induce lower forces than at approach or take-off speed (same vortex strength, same aircraft, same configuration). Additionally, any turbulence or even upset is far less dangerous in cruise as ground clearance is suffcient to counteract and small deviations from planned flight-path is less of concern.

    in reply to: Boeing's big test a success #590519
    Schorsch
    Participant

    Thank you, Bmused55.

    We should especially be happy that there are two companies working profitable and developing technology. Both employing lots of people, mostly in our homecountries (so not somewhere in Kokonistan), strenghening local economy.
    We should try to see the big picture: Airbus has gained much ground since mid 1990s, but still 80% of in-service aircraft are Boeing. Hence they are better positioned on the market. If Airbus gets 40% market share in a growing market, pas de probléme!

    And we should understand complexity of business and new business solutions, as well as marketing effort or just erroneous attemps. I see Airbus and I tell you: Lots of room for improvement.

    But: If I read one-sided article and posts, I answer with one-sided! 🙂

    in reply to: Boeing's big test a success #591186
    Schorsch
    Participant

    Bmused, you’re right. I took a cheap hit. Mostly because I was annoyed by the simple attitude of the posted article. I am working for Airbus, so please apologize that I am biased. I however agree with you in two important points:

    1
    Boeing may and in my perception will deliver more airplanes than Airbus at least from 2008 on (if 787 goes as planned). That is a fact and I don’t consider it a “defeat” (I don’t even see a battle).

    2
    Airbus is doing similar business strategies as Boeing, in my perception with lower amplitude. Airbus is not outsourcing its production as Boeing does. Once again, the article was somehow ‘cheap’, hence my reply also ‘cheap’.

    I think that this A vs B thing will become different in some years. We will see both companies going shoping around the world to get their aircrafts together. The opinion that Boeing is American and Airbus is European is outdated. The American workshare on an A380 can be similar to that of an B787 if the according variants are chosen.

    So, to make it short: I try to be rational. Articles like the posted one let me get ‘irrational’.

    in reply to: Boeing's big test a success #591359
    Schorsch
    Participant

    The storied American planemaker strongly outsold archrival Airbus SAS this year, setting course to recapture the title Boeing owned until Airbus snatched it away two years ago: world’s biggest aircraftmaker.

    ‘biggest’? Measured by layed off workers or newly hired marketing staff? Calling you the biggest aircraftmaker you actually need to make aircraft! Just getting an order doesn’t count.

    Airbus delivered more aircraft this year. Looking at Boeing’s business model Boeing will never get again a ‘big’ company, but a ‘big’ “system intergrator”.

    Maybe the 797 will be build by a consortium of GE, Vought and Mitsubishi Heavy Industries. Boeing sells the name and becomes as unique as ‘Jeep’, ‘Buick’ or ‘Lexus’.

    in reply to: Boeing's big test a success #591360
    Schorsch
    Participant

    US Agent,
    you seem very focussed in determing a ‘winner’ of a ‘battle’. Fact is, that the A380 is flying. It is experiencing problems, which are all solvable in reasonable time and cost (believe, I’m working on it). True is, it was planned different by cost-concerned Airbus managers.

    And here comes the lesson: Do not celebrate victory before your plane is flying. The 787 is sure a good design, but hasn’t even lifted off not speaking of certification or revenue service.

    My advice: Just be happy, be excited, but do not predict something on the limited facts you have. Only do it if you want to emberasse yourself due to wrong predictions. Building an airplane is such a difficult task, Boeing promised the final marvel to the airlines and, at the same time, re-invented the Boeing Company to a organization that does not reflect its employees wishes (no enginees likes to divert activities to Russia and lay off his buddies). I wish best luck to Boeing. The will need some of it.

    Your 4 points in the end are BS. And, please believe me, if Airbus would have won all 4 I would call it BS, too.

    in reply to: VLA sensitivity to wakes #591752
    Schorsch
    Participant

    It’s always easier to blame the dead guy in order keep the living (persons/company) clear of the inevitable lawsuits. Plus, we’ve yet to see a dead pilot be able to speak on his own behalf. Instead, we have hundreds, if not thousands, of “experts” judging the actions of a few in perfect hindsight. Nothing like a board of suits spending years to judge an action that someone had only seconds to comprehend let alone react to.

    Sorry, I do not know the pilot (not even his name). I just draw my conclusions from the available information. I do not judge the pilot as an individuum, I just judged him as pilot. And in this function, he certainly did a fatal mistake and, as I said, that was partly contributed by AA training and A300-600 rudder control mechanism. Those “experts” actually are experts. The pilot misjudged? Why did he do it? Read the report!

    I agree with you.
    This is why American Airlines are bitterly defending their pilot.
    Its because of all this, I reserve judgement on who or what was responsible.

    American law suit resulted in a 95%-share of “financial responsibility” for AA. Maybe all the high-paid lawyers did not get it right? Don’t you think that if there was any possibility of blaming Airbus of the accident they would have tried it. After all, I in the first place blame AA and not the individual pilot for that accident.

    Exactly how many miles behind the 747-400 was the Airbus 300 when wrecked?

    Please, the aircraft wasn’t wrecked by the vortex but by the pilot (or if somebody wants to believe by the faulty VTP, but definitly not the vortex). AA587 was about 120 seconds behind the Japan Airlines B747. Vortex decays with time, not distance. ICAO recommandations quoted are for approach/take-off. Seperation grows for cruise, although cruise vortex encounter is far less dangerous (and therefore normally not mentioned).

    in reply to: VLA sensitivity to wakes #594692
    Schorsch
    Participant

    Airbus say the pilot acted wildly, American say he did what he was trained to do.

    So there is no way you or I can sayfor sure who is to blame. Personaly I say both parties have responsibility. Although to Airbus’ credit, the tail didn’t snap till around 130% designed max load.

    I would orientate myself on the official report of the NTSB that clearly states that
    – the co-pilot was responsibly due to “excessive and unnecessary” rudder inputs
    – the training of AA contributed to the accident
    – the rudder control system contributed to the accident

    The tail withstood 1.9 times the limit load, that is the maximum allowed load on vertical tail. The structure behaved exactly as Airbus predicted and NTSB stated that in the report. The rudder travel limiter was object heavy criticism by authorities and the reason why AA blamed Airbus as responsible. However, the limiter is not well designed and tricky to handle, but was certified.

    Hence we can clearly conclude who is responsible.

    in reply to: VLA sensitivity to wakes #594899
    Schorsch
    Participant

    As Airbus and American Airlines are painfully aware of! (although that was more the tail fin)

    While in this case the vortex did not cause anything like strutural damage or aircraft upset. It just triggered the wild behaviour of the co-pilot.

    in reply to: VLA sensitivity to wakes #594910
    Schorsch
    Participant

    Large aircraft are still sensitive to wakes. I remember seeing a few pictures of 707’s and DC-8’s who had engines removed by the wakes of similar aircraft they were following. Sure, the dangers for a 747 are different than a C152 but there are still risks.

    Isn’t only the 753 considered a Heavy aircraft? I believe I have also heard the Heavy callsign for 739’s as well but I could be mistaken. I know there was an attempt to get the 737NG’s recategorized as the wakes off their new wings packed quite a punch when compared to the previous 737’s. I know the few times I’ve gotten rocked rather hard by a previous airplanes wake it was reported as a 738 or 739.

    I actually concentrated more on the aircraft as rigid-body system. But you are right: A high-energy vortex may cause structural damage at large aircraft. Especially parts like vertical tail plane.

    in reply to: VLA sensitivity to wakes #595421
    Schorsch
    Participant

    Has Boeing ever tried to prove that a B757 does not produce such strong vortices and is not heavy?

    Also, how sensitive is a B757 to the wake vortices of B747? Or of another B757?

    Please define a scenario and “sensitivity”. B757-pilots will surely not want to take of directly after a B747. Encounters are very frequent in today’s business, some really getting close to “upset recovery”´. The best documented incident (AA587 in NY November 2001) was not really a big encounter.

    in reply to: VLA sensitivity to wakes #595439
    Schorsch
    Participant

    The impact of a Wake Vortex Encounter is dependend on:
    – aircraft’s span
    – inertia
    – airspeed
    – mass
    The higher inertia will reduce the effects of rolling. The size will maybe result in encountering both vortices at the same time. Generally I think the effect is neglitible.

    @Bmused55: Be aware about the preliminary status of the ICAO-recommendation. The seperation categories by ICAO are outdated and not appropriate at all. The understanding of wake vortex generation is limited. We will see a totally new approach developing over the next years. After being threatened by ICAO with the increased seperation, Airbus is doing research in order to prove that A380 will have only slightly increased vortex. Additionally, the A380’s climb performance will enable it to clear the airspace faster than a B747.
    This research was not conducted before because nobody was really interested. The (sorry to say it this hard) propaganda of Boeing, that A380 will nullify its slot-advantage, is embarassing for such an old company. I actually believe that they have no idea what kind of vortices their own aircraft produce.

    Just to add: Category heavy starts at 136 tons (including everything from a A310 to a B747-400). A B757 is actually rated as “heavy”, too, because it produces such strong vortices. Taking the ICAO-seperation as proven fact is scientificly not valid.

    in reply to: B737 vs. A32X #596177
    Schorsch
    Participant

    If you compare the needs of different 737/32X customers, you’ll find a variety of needs. The only take these models because it is the best you can get. The big market and diverse needs in a competive situation calls for a diversification.
    Second, developments in public opinion, oil prices and environmental concerns may totally change the market place and anybody who rushs to build a modestly improved singe aisle aircraft may find himself coming up with the wrong product. I saw studies for unswept-wing overwing-engine designs as well as large turbo-props, and conventional designs.
    We will see lots of discussion about this issue as soon as the longe-range-happy battles of A&B have ceased. We will possibly also see that A&B partly withdraw from the market because the margins are too low.

    in reply to: B737 vs. A32X #596343
    Schorsch
    Participant

    Would they be able to increase the speeds without affecting the fuel efficiency in future for the replacement aircrafts like 320/737 etc..

    Is there a technically availaible viable solution for this?

    No, I doubt that. The way to go is more the other way round: reduce speed and gain weight-saving and reduced fuel consumption. A speed reduction to M0.7 or M0.65 would cost you some minutes but most time you spend in taxiing, take-off and landing. All those are restricted in temrs of speed.

    As I tried to explain to Bmused it is this not just as it is with previous porgrams. The manufacturers will have to go very deep inside the topic and evaluate the costs of all aspects of operation. Ths will maybe cause a diversification of the market with Bombardier, the Russians, Embrear or even the Chinese entering the market.
    Definetly the market for single-aisle will be completly different than that for B787 or even A380. The single-aisle airliner will stay less sophisticated and development of a competitive design is achievable by other companies than A&B.
    That is actually what I read out of the quote from the Boeing guy, just filter out the US-typical adjectives and you can find my statements in it.

Viewing 15 posts - 3,451 through 3,465 (of 3,480 total)