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A gas turbine engine is mounted on an aircraft which can attain a maximum altitude of $11 \mathrm{~km}$ from sea level. The combustor volume of this engine is decided based on conditions at
(A) sea level
(B) $8 \mathrm{~km}$ altitude
(C) $5.5 \mathrm{~km}$ altitude
(D) $11 \mathrm{~km}$ altitude


Question ID - 156016 | Toppr Answer

A gas turbine engine is mounted on an aircraft which can attain a maximum altitude of $11 \mathrm{~km}$ from sea level. The combustor volume of this engine is decided based on conditions at
(A) sea level
(B) $8 \mathrm{~km}$ altitude
(C) $5.5 \mathrm{~km}$ altitude
(D) $11 \mathrm{~km}$ altitude

1 Answer - 5876 Votes

3537

Answer Key : (D) -

(D) $11 \mathrm{~km}$ altitude



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