IDC PENERBANGAN, di mana mengangkut

IDC PENERBANGAN, di mana mengangkut kendaraan dapat beroperasi. Koridor dibatasi oleh batas angkat, batas suhu, dan batas kekuatan aerodinamis. Batas angkat ditentukan oleh ketinggian tingkat-penerbangan maksimum pada kecepatan tertentu. batas suhu diatur oleh batas termal struktural dari bahan yang digunakan dalam konstruksi pesawat. Pada setiap ketinggian tertentu, kecepatan maksimum mencapai suhu-dibatasi oleh efek pemanasan aerodinamis. Pada ketinggian rendah, kecepatan dibatasi oleh beban gaya aerodinamika bukan oleh suhu Daerah operasi semua pesawat kebohongan dalam koridor penerbangan. Wilayah operasi dari pesawat tertentu dalam koridor ditentukan oleh desain pesawat, tapi itu sangat sebagian kecil dari koridor keseluruhan

Hasil (Inggris) 1:

IDC FLIGHTS, where transport vehicles can operate. The corridor is limited by the boundaries of lift, limit temperature, and limit the power of aerodynamics. Lift limit is determined by the maximum flight altitude level-at a given speed. the limit temperature is regulated by the thermal limit of the structural materials used in aircraft construction. At any particular altitude, maximum speed is reached the temperature-constrained by the warming effect of aerodynamics. At low altitude, the speed is limited by the load temperature is not aerodynamics by style regions of operation all aircraft lies in the flight corridor. Area of operation of certain aircraft in the corridors defined by the design, but it's a very small portion of the overall corridor

Hasil (Inggris) 2:

FLIGHT IDC, where transport vehicles can operate. Corridor bounded by lifting limits, temperature limits, and the limits of aerodynamic force. Lift height limit is determined by the maximum flight level at a certain speed. temperature limit is set by the thermal limits of the structural materials used in aircraft construction. At any given height, the maximum speed reaches a temperature-limited by the effects of aerodynamic heating. At low altitude, the speed is limited by the weight of the aerodynamic forces rather than by temperature Operating area all lie in the aircraft flight corridors. Area of ​​operation of certain aircraft in the corridors defined by the design of aircraft, but it was very small part of the overall corridor