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GATE Aerospace Engineering Engineering Mathematics Flashcards

51 question-and-answer cards covering Engineering Mathematics as it is examined in GATE Aerospace Engineering. 24 of them are printed below, taken from across the deck — no signup, no paywall on the preview.

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24 sample cards from the Engineering Mathematics deck

Sampled from the end of the deck, so these are different cards from the ones shown on the syllabus page.

  1. State the chain rule for $y=f(g(x))$.

    $\dfrac{dy}{dx}=f'(g(x))\cdot g'(x)$, i.e. $\dfrac{dy}{dx}=\dfrac{dy}{du}\cdot\dfrac{du}{dx}$ with $u=g(x)$.

  2. Define the partial derivative $\frac{\partial f}{\partial x}$ of $f(x,y)$.

    $\dfrac{\partial f}{\partial x}=\lim_{h\to 0}\dfrac{f(x+h,y)-f(x,y)}{h}$ — differentiate with respect to $x$ holding $y$ constant.

  3. State the total differential of $z=f(x,y)$.

    $dz=\dfrac{\partial f}{\partial x}\,dx+\dfrac{\partial f}{\partial y}\,dy$.

  4. What is the necessary (first-order) condition for a local extremum of $f(x,y)$?

    Both first partial derivatives vanish: $\dfrac{\partial f}{\partial x}=0$ and $\dfrac{\partial f}{\partial y}=0$, giving a stationary (critical) point.

  5. State the second-derivative (Hessian) test for $f(x,y)$ at a critical point using $D=f_{xx}f_{yy}-f_{xy}^{2}$.

    If $D>0$ and $f_{xx}>0$: local minimum. If $D>0$ and $f_{xx}<0$: local maximum. If $D<0$: saddle point. If $D=0$: test inconclusive.

  6. For a single-variable function, give the second-derivative test for maxima and minima.

    At a critical point $x_{0}$ where $f'(x_{0})=0$: if $f''(x_{0})>0$ it is a local minimum; if $f''(x_{0})<0$ it is a local maximum; if $f''(x_{0})=0$ the test fails.

  7. Define the gradient of a scalar field $\phi(x,y,z)$ and state its physical meaning.

    $\nabla\phi=\dfrac{\partial\phi}{\partial x}\hat{i}+\dfrac{\partial\phi}{\partial y}\hat{j}+\dfrac{\partial\phi}{\partial z}\hat{k}$. It points in the direction of maximum rate of increase of $\phi$ and is normal to level surfaces $\phi=$ const.

  8. Define the divergence of a vector field $\vec{F}=(F_1,F_2,F_3)$ and its physical meaning.

    $\nabla\cdot\vec{F}=\dfrac{\partial F_1}{\partial x}+\dfrac{\partial F_2}{\partial y}+\dfrac{\partial F_3}{\partial z}$ (a scalar). It measures the net outward flux per unit volume (source/sink strength).

  9. Define the curl of a vector field $\vec{F}$.

    $\nabla\times\vec{F}=\begin{vmatrix}\hat{i}&\hat{j}&\hat{k}\\ \partial_x&\partial_y&\partial_z\\ F_1&F_2&F_3\end{vmatrix}$ (a vector measuring local rotation/circulation of the field).

  10. State the standard identities $\nabla\times(\nabla\phi)$ and $\nabla\cdot(\nabla\times\vec{F})$.

    $\nabla\times(\nabla\phi)=\vec{0}$ (curl of a gradient is zero) and $\nabla\cdot(\nabla\times\vec{F})=0$ (divergence of a curl is zero).

  11. What is a solenoidal field and what is an irrotational (conservative) field?

    Solenoidal: $\nabla\cdot\vec{F}=0$ (no sources/sinks). Irrotational: $\nabla\times\vec{F}=\vec{0}$, meaning $\vec{F}=\nabla\phi$ for some scalar potential $\phi$.

  12. State the formula for the directional derivative of $\phi$ in the direction of unit vector $\hat{u}$.

    $D_{\hat{u}}\phi=\nabla\phi\cdot\hat{u}$. It is maximum (equal to $|\nabla\phi|$) when $\hat{u}$ is along $\nabla\phi$.

  13. State the fundamental theorem of calculus relating the definite integral to an antiderivative.

    If $F'(x)=f(x)$, then $\displaystyle\int_{a}^{b}f(x)\,dx=F(b)-F(a)$.

  14. State the integration by parts formula.

    $\displaystyle\int u\,dv=uv-\int v\,du$.

  15. Define a line integral of a vector field $\vec{F}$ along a curve $C$ and what it represents.

    $\displaystyle\int_{C}\vec{F}\cdot d\vec{r}$, representing the work done by $\vec{F}$ along $C$. For a conservative field $\vec{F}=\nabla\phi$ it equals $\phi(\text{end})-\phi(\text{start})$ and is path-independent.

  16. Write the surface integral expressing the flux of $\vec{F}$ through a surface $S$.

    $\displaystyle\iint_{S}\vec{F}\cdot\hat{n}\,dS=\iint_{S}\vec{F}\cdot d\vec{S}$, where $\hat{n}$ is the outward unit normal.

  17. State Green's theorem in the plane.

    $\displaystyle\oint_{C}(P\,dx+Q\,dy)=\iint_{R}\left(\dfrac{\partial Q}{\partial x}-\dfrac{\partial P}{\partial y}\right)dx\,dy$, where $C$ is the positively oriented boundary of region $R$.

  18. State the Gauss (divergence) theorem.

    $\displaystyle\iint_{S}\vec{F}\cdot\hat{n}\,dS=\iiint_{V}(\nabla\cdot\vec{F})\,dV$, converting outward flux through closed surface $S$ into a volume integral over $V$.

  19. State Stokes' theorem.

    $\displaystyle\oint_{C}\vec{F}\cdot d\vec{r}=\iint_{S}(\nabla\times\vec{F})\cdot\hat{n}\,dS$, where $C$ is the boundary curve of surface $S$.

  20. Compare Green's, Stokes', and Gauss' theorems by what they relate.

    Green: line integral around a plane curve to a double (area) integral. Stokes: line integral around a space curve to the surface integral of the curl (3-D generalization of Green's). Gauss: closed surface flux integral to a volume integral of the divergence.

  21. What makes a first-order ODE $\frac{dy}{dx}=f(x,y)$ separable, and how is it solved?

    It is separable if it can be written $g(y)\,dy=h(x)\,dx$. Solve by integrating both sides: $\int g(y)\,dy=\int h(x)\,dx + C$.

  22. Give the standard form of a first-order linear ODE and its integrating factor.

    $\dfrac{dy}{dx}+P(x)\,y=Q(x)$ with integrating factor $\mu=e^{\int P\,dx}$. Solution: $y\,\mu=\displaystyle\int Q\,\mu\,dx + C$.

  23. What is the condition for the first-order ODE $M\,dx+N\,dy=0$ to be exact, and what is its solution form?

    Exact iff $\dfrac{\partial M}{\partial y}=\dfrac{\partial N}{\partial x}$. Then there exists $u(x,y)$ with $\dfrac{\partial u}{\partial x}=M,\ \dfrac{\partial u}{\partial y}=N$, and the solution is $u(x,y)=C$.

  24. What is a Bernoulli equation (a first-order nonlinear ODE) and how is it reduced to linear form?

    $\dfrac{dy}{dx}+P(x)y=Q(x)y^{n}$, $n\neq 0,1$. Substitute $v=y^{1-n}$, which transforms it into the linear ODE $\dfrac{dv}{dx}+(1-n)P(x)v=(1-n)Q(x)$.

What this deck covers

The Engineering Mathematics deck follows the GATE Aerospace Engineering Engineering Mathematics syllabus — 4 chapters and 26 topics — so questions land on material that is genuinely examinable rather than trivia around it. That works out to roughly 12.8 cards per chapter.

Answers are written to be recallable, not just readable — averaging about 151 characters, which is long enough to carry the reasoning and short enough to say out loud.

A deck like this earns its keep on the second and third pass. Read the syllabus first so you know the shape of the subject, then use the cards to find the specific facts that have not stuck.

Engineering Mathematics flashcards FAQ

How many Engineering Mathematics flashcards are in this GATE Aerospace Engineering deck?

51 cards. This page previews 24 of them, sampled evenly across the deck so you can judge the difficulty before installing anything.

Are these GATE Aerospace Engineering flashcards free?

Yes. The preview here is free to read with no signup, and the full 51-card deck is free inside the Examius app.

What do the Engineering Mathematics cards cover?

They follow the GATE Aerospace Engineering Engineering Mathematics syllabus — 4 chapters and 26 topics — so the questions track what is actually examinable.

How should I use these flashcards?

Read the syllabus first so you know the shape of the subject, then drill the deck. Examius schedules each card with spaced repetition, so cards you keep missing come back sooner and ones you know drift further apart.