Topic: Selection of a suitable aerofoil is critical to the performance of the UAV.< Requirement: Maximum Wing-Span: 5 m Maximum Cruise Speed (altitude of 250 m): 200 km/hr Total Mass of UAV: 12 kg< Consideration of flaps for take-off and landing Define Key Requirements: ( Determine the design mission profile, including take-off, landing, and cruising phases.< Decide on the take-off and landing speeds.<
Topic: Selection of a suitable aerofoil is critical to the performance of the UAV.< Requirement: Maximum Wing-Span: 5 m Maximum Cruise Speed (altitude of 250 m): 200 km/hr Total Mass of UAV: 12 kg< Consideration of flaps for take-off and landing Define Key Requirements: ( Determine the design mission profile, including take-off, landing, and cruising phases.< Decide on the take-off and landing speeds.<
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Transcribed Image Text:Topic: Selection of a suitable aerofoil is critical to the performance of the UAV.<
Requirement:
Maximum Wing-Span: 5 m
Maximum Cruise Speed (altitude of 250 m): 200 km/hr
Total Mass of UAV: 12 kg<
Consideration of flaps for take-off and landing
له
Define Key Requirements:<
لے
Determine the design mission profile, including take-off, landing, and cruising phases.<
Decide on the take-off and landing speeds.
Determine the desired lift coefficient and drag characteristics for each flight phase.<
له
Create a sample calculation
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Step 1: Determine design mission profile, the take-off and landing speeds, and desired lift coefficient.
VIEWStep 2: Find design machine profile
VIEWStep 3: Calculate take off and landing speed
VIEWStep 4: find the desired lift coefficient and drag characteristics for each flight phase.
VIEWStep 5: sample calculations
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