Aircraft Performance(Aerospace And Aeronautical ) Questions and Answers
Explanation:-
Answer: Option D. -> coverage of distanceCIVILIAN AIRCRAFT MAINLY FOCUSES ON DISTANCE COVERAGE. CIVILIAN AIRCRAFT LOOKS FOR MAKING PROFIT BY MANAGING FUEL CONSUMPTION. THIS IS BECAUSE IT DOESN’T NEED TO PERFORM ANY ATTACKING MANEUVERS. A CIVILIAN AIRCRAFT IS MORE PREFERRED WHEN IT GIVES GUARANTEED SAFETY FOR THE PASSENGERS AND ALSO BY OFFERING LUXURY FACILITIES.
Explanation:-
Answer: Option A. -> TrueTHERE ARE TWO TYPES OF MISSION PROFILES. THEY ARE CIVILIAN MISSION PROFILE AND MILITARY MISSION PROFILE. A CIVILIAN MISSION PROFILE FOCUSES ON FUEL CONSUMPTION AND DISTANCE COVERED WHEREAS A MILITARY MISSION PROFILE FOCUSES ON ENDURANCE AND SPEED.
Explanation:-
Answer: Option C. -> high altitude and cover long distanceTHE PURPOSE OF SURVEILLANCE AIRCRAFT IS TO MAINTAIN HIGH ALTITUDE AND COVER AN ESTIMATED DISTANCE OF FLIGHT IN THE GIVEN PERIOD OF TIME. A SURVEILLANCE AIRCRAFT DOESN’T NEED TO PERFORM ANY KIND OF MANEUVERING OR ATTACK OTHER AIRCRAFTS.
Explanation:-
Answer: Option B. -> FalseA MILITARY AIRCRAFT IS NOT DESIGNED TO BE LUXURIOUS AND ENTERTAINING. MILITARY AIRCRAFT MAINLY FOCUSES ON MILITARY MANEUVERS. A MILITARY AIRCRAFT IS GENERALLY PREFERRED TO MAINTAIN HIGH ALTITUDE AND PERFORM VARIOUS MILITARY MANEUVERS AT HIGHER ALTITUDES.
Explanation:-
Answer: Option D. -> Short take-off and vertical landingTHE FULL FORM OF STVOL IS SHORT TAKE-OFF AND VERTICAL LANDING. MOSTLY FIXED-WING AIRCRAFTS COME UNDER THIS CATEGORY. STOVL PERFORMANCE OF AN AIRCRAFT IS THE ABILITY OF AN AIRCRAFT TO TAKE OFF AND CLEAR A 50-FOOT OBSTRUCTION IN A DISTANCE OF 1,500 FEET FROM BEGINNING THE TAKEOFF RUN AND LAND VERTICALLY.
Explanation:-
Answer: Option A. -> Short take-off and landingTHE FULL FORM OF STOL IS SHORT TAKE-OFF AND LANDING. STOL MUST ALSO BE ABLE TO STOP WITHIN 1,500 FEET AFTER CROSSING A 50-FOOT OBSTACLE ON LANDING. THIS KIND OF LANDING IS HELPFUL IN HARSH LANDING.
Explanation:-
Answer: Option A. -> Decrease in climb performanceTHERE WILL BE A DECREASE IN CLIMB PERFORMANCE WITH INCREASE IN HIGH DENSITY ALTITUDE. ON INCREASE OF ALTITUDE THERE WOULD BE A DECREASE IN DENSITY WHICH RESULTS IN DECREASE IN POWER OUTPUT OF ENGINE AND AIRFOIL EFFICIENCY, AS A RESULT THERE WILL BE A DECREASE IN CLIMB INCREASE PERFORMANCE.