In gliding (unpowered) flight, the lift and drag are in equilibriumwith the weight. Show that if there is no wind, theaircraft sinks at an angletan θ ≈drag/liftFor a sailplane of mass 200 kg, wing area 12 m2, and aspectratio 11, with an NACA 0009 airfoil, estimate (a) the stallspeed, (b) the minimum gliding angle, and (c) the maximumthe distance it can glide in still air when it is 1200 mabove level ground.

The force of weight is balanced out by both drag and lift force, where the drag force acts in the…

Answered: In gliding (unpowered) flight, the lift…

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

Related questions

Concept explainers

Question

In gliding (unpowered) flight, the lift and drag are in equilibrium
with the weight. Show that if there is no wind, the
aircraft sinks at an angle
tan θ ≈drag/lift
For a sailplane of mass 200 kg, wing area 12 m², and aspect
ratio 11, with an NACA 0009 airfoil, estimate (a) the stall
speed, (b) the minimum gliding angle, and (c) the maximum
the distance it can glide in still air when it is 1200 m
above level ground.

Expert Solution

Trending now

This is a popular solution!

Step by step

Solved in 3 steps with 11 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

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.

Similar questions