Homework Help is Here – Start Your Trial Now!
Engineering
Mechanical Engineering
An aircraft has a total mass of (1.18x10^2) kg and a wing area of (2.700x10^1) m². It operated with an aerofoil section having CL = 1.0 and Cp=0.1. Assuming that the total drag of the wing represents the whole drag of the aircraft, find the power input required for to overcome gravity and take off. Assume density of air to be 1.2 kg/m3. Answer should be in Watts with three significant figures.

An aircraft has a total mass of (1.18x10^2) kg and a wing area of (2.700x10^1) m². It operated with an aerofoil section having CL = 1.0 and Cp=0.1. Assuming that the total drag of the wing represents the whole drag of the aircraft, find the power input required for to overcome gravity and take off. Assume density of air to be 1.2 kg/m3. Answer should be in Watts with three significant figures.

Elements Of Electromagnetics
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
See similar textbooks
icon
Related questions
Question
Need the answer with working out. Thanks
An aircraft has a total mass of (1.18x10^2) kg and a wing area of (2.700x10^1) m². It operated with an aerofoil section having CL represents the whole drag of the aircraft, find the power input required for to overcome gravity and take off. Assume density of air to be 1.2 kg/m. Answer should be in Watts with three significant figures. = 1.0 and Cp=0.1. Assuming that the total drag of the wing Note: Your answer is assumed to be reduced to the highest power possible. Your Answer: x10 Answer SW 36 DOLL PrtScr Insert Home A F11 F12 F8 F9 F10 F4 F5 F6 F7 F3 & $4
Transcribed Image Text:An aircraft has a total mass of (1.18x10^2) kg and a wing area of (2.700x10^1) m². It operated with an aerofoil section having CL represents the whole drag of the aircraft, find the power input required for to overcome gravity and take off. Assume density of air to be 1.2 kg/m. Answer should be in Watts with three significant figures. = 1.0 and Cp=0.1. Assuming that the total drag of the wing Note: Your answer is assumed to be reduced to the highest power possible. Your Answer: x10 Answer SW 36 DOLL PrtScr Insert Home A F11 F12 F8 F9 F10 F4 F5 F6 F7 F3 & $4
Expert Solution
steps

Step by step

Solved in 2 steps

SEE SOLUTIONCheck out a sample Q&A here
Blurred answer
Knowledge Booster
Quality Assurance, Process Planning, and Quality Control
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Recommended textbooks for you
Elements Of Electromagnetics
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY
SEE MORE TEXTBOOKS