Aerospace Engineering
GATE AE concept:steady-climb PYQs
Build your understanding with focused practice from past exam papers.
How to practice concept:steady-climb
Attempt a question, record the concept and assumptions, then check the available answer. Rework mistakes after revising the relevant concepts. Topic tags can overlap; review the question context.
Questions 1–2 of 2. Imported answers require independent review unless marked reviewed.
Question 59
Open questionAENAT2 marksNeeds review
An airplane with wing planform area of 20 m
and weight 8 kN is flying straight and level with a speed of 100 m/s. The total drag coefficient is 0.026 and the air density is 0.7 kg/m
. The total thrust required to introduce a steady climb angle of 0.1 radians is ___ N. (round off to the nearest integer)Log in to check the answer
You can attempt this question now. Sign in to view the answer key, explanations and discussion.Log in to check answerQuestion 43
Open questionAENAT2 marksNeeds review
An aircraft is to be designed to ensure that it has enough excess power to achieve steady climb at flight path angle,
degrees, maintaining
. The numerical value of the thrust to weight ratio of the complete aircraft to meet the above requirement under standard atmospheric condition will be ________ (in three decimal place).Log in to check the answer
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