1. 26.
    0
    @19 pm atayım mı la ibine
    ···
  2. 27.
    0
    isim ver bin
    ···
  3. 28.
    0
    @22 ehmmm şey olsun müella
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  4. 29.
    0
    5 satırdan uzunsa olmaz hocu
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  5. 30.
    0
    @24 ayar çekeriz sen çevirecem de yeter olmadı gibertirsin aradan bir iki cümle koduğum
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  6. 31.
    0
    sol taŞaktan düşüyoz binler up up up
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  7. 32.
    0
    bune amk miğdem kalktı
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  8. 33.
    0
    müella dedikya oç
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  9. 34.
    0
    what the fucking going on here ?
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  10. 35.
    0
    la üstümdeki gibik help me la
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  11. 36.
    0
    amk ben de o aynştaynın günlüğü çevirilcek sandım. sen bi gibim koymamışsın ki buraya
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  12. 37.
    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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  13. 38.
    0
    are you joke? get age!!!
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  14. 39.
    0
    bu da teslanın mı hangi gibimin günlüğü amk çok uzun
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  15. 40.
    +1
    summarize it bastard
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  16. 41.
    0
    @36 hi mrs smith. can we go to the seaside?
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  17. 42.
    0
    fuck you
    ···