tümü

ingilizcem var diye hava atan piçler

  1. 1.
    +1
    size paragraf vereyim de çevirin... gibtiğimin dünyasında bir işe yaramış olun amk
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    #4861228 şikayet
  2. 2.
    0
    sol taşşaktan düşmeden hedeleyin giberim
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    #4861261 şikayet
  3. 3.
    0
    @2 yollayayım mı la bi paragraf pm den bin?
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    #4861288 şikayet
  4. 4.
    0
    @5 yeah, sevişelim mi?
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    #4861300 şikayet
  5. 5.
    0
    @8 bilion mu la? zütü gibik
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    #4861331 şikayet
  6. 6.
    0
    @15 gibtir git kendi gibimtrak entry ni gir zütoğlanı
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    #4861450 şikayet
  7. 7.
    0
    @18 para köpeğin olsun sidikli
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    #4861508 şikayet
  8. 8.
    0
    @19 pm atayım mı la ibine
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    #4861523 şikayet
  9. 9.
    0
    @22 ehmmm şey olsun müella
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    #4861614 şikayet
  10. 10.
    0
    @24 ayar çekeriz sen çevirecem de yeter olmadı gibertirsin aradan bir iki cümle koduğum
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    #4861661 şikayet
  11. 11.
    0
    sol taŞaktan düşüyoz binler up up up
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    #4861706 şikayet
  12. 12.
    0
    müella dedikya oç
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    #4861738 şikayet
  13. 13.
    0
    la üstümdeki gibik help me la
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    #4861819 şikayet
  14. 14.
    0
    gas turbines are rated for a power output level (horsepower or
    megawatts) at a temperature and altitude condition. two standards
    used are the international standards organization (iso) and the
    national electrical manufacturers association (nema). iso conditions
    are defined as 59°f inlet temperature, 14.7 psia inlet pressure,
    and 60% relative humidity, and nema conditions are defined as 80°f
    inlet temperature and 1,000-foot elevation. for surface applications, a
    rating curve showing power vs. inlet temperature is widely used (figure 5-3). this power curve is influenced by four distinct factors: inlet
    air temperature, turbine inlet temperature (i.e., combustor discharge
    temperature), rotor speed(s), and compressor aerodynamics.
    turbine inlet temperature is a limiting factor in all gas turbines,
    regardless of design configuration. this limit has been extended
    through utilization of internal turbine airfoil cooling. limitations due
    to speed and compressor aerodynamics are distinguished as break
    points or slope changes in the power curve. often, these limitations
    are of little consequence since they are small relative to the turbine
    inlet temperature limitations. the effects of increasing ambient temperature
    on gas turbine output clearly indicate the advantages of
    cooling the compressor inlet, especially in hot climates. lowering the
    compressor inlet temperature can be accomplished by the installation
    of an evaporative cooler, a fogger system, or a chiller in the inlet ducting

    al la çevir şukuya boğacam seni @31
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    #4861902 şikayet