Question:medium

Which of the following sequences correctly represents the flow of air in a basic turbojet engine?

Show Hint

The complete turbojet flow sequence is \[ \boxed{ \text{Intake} \rightarrow \text{Compressor} \rightarrow \text{Combustor} \rightarrow \text{Turbine} \rightarrow \text{Nozzle}. } \] If the compressor is omitted in the options, choose the remaining components in the same order.

Updated On: Jul 14, 2026

Nozzle \(\rightarrow\) Combustor \(\rightarrow\) Intake \(\rightarrow\) Turbine
Intake \(\rightarrow\) Combustor \(\rightarrow\) Turbine \(\rightarrow\) Nozzle
Turbine \(\rightarrow\) Nozzle \(\rightarrow\) Intake \(\rightarrow\) Combustor
Combustor \(\rightarrow\) Intake \(\rightarrow\) Nozzle \(\rightarrow\) Turbine

Show Solution

The Correct Option is B

Solution and Explanation

Was this answer helpful?

0

Top Questions on Aircraft Engines

Questions Asked in TS PGECET exam

The Eigenvalues of \(3\times 3\) real matrix A are 1, 2, 3 then \(A^{-1} =\)

TS PGECET - 2026
Linear Algebra

Let \(A=\begin{bmatrix} 1 & 1 & 0 \\ 0 & 1 & 1 \\ 0 & 0 & 1 \end{bmatrix}\). If \(u_1\) and \(u_2\) are column matrices such that \(Au_1 = \begin{bmatrix} 2 \\ 1 \\ 0 \end{bmatrix}\) and \(Au_2 = \begin{bmatrix} 1 \\ 0 \\ 1 \end{bmatrix}\), then \(u_1 - u_2\) is

TS PGECET - 2026
Matrices

Let \(a,b\) and \(c\) be real numbers. Suppose there exist real numbers \(x,y,z\) which are not all zero such that the system of equations \(x = cy + bz\), \(y = cx + az\) and \(z = bx + ay\) has a non-zero solution then \(\left(a+b+c\right)^2 =\)

TS PGECET - 2026
Determinants

For the function \(f(x)=\log x\), the number \(c\) strictly between \(e^2\) and \(e^3\) that satisfies \(f'(c)=\dfrac{f(e^3)-f(e^2)}{e^3-e^2}\) is

TS PGECET - 2026
Calculus