Guest
You need to login to ask any Questions from chapter Flow-Past-Through-Submerged-Body of Fluid-Mechanics

Chapter:

Flow-Past-Through-Submerged-Body

A kite has an effective area of `0.6 m^2` and mass 0.4 kg. It experience a drag of 15 N in a wind speed of 40 km/hr. Determine
tension in chord if it makes an angle of `45^0` with horizontal.

lift coefficient for kite
Consider density of air as 1.2 kg/`m^3`. [2070-Ashad ][8]

Previous Question

Next Question

All Chapters

View all Chapter and number of question available From each chapter from Fluid-Mechanics

Dimensional Analysis, Similitude and Physical Modelling

Complete IOE exam solution including with important theory and numerical solution

Flow Past Through Submerged Body

Complete IOE solution including important theory and numericals

Boundary Layer Theory

Complete IOE exam solution and many important theory and numericals

Properties of fluid

properties of fluids
complete IOE solution on fluid mechanics
Detailed description chapterwise
Unlimited Numericals problem solved with updation daily
And much more

Hydrostatics

Hydrostatics basic theory
All important Numericals
IOE,PU, MIT,A.M.I.E,Delhi university,EUPS,Engineering service exam solved problems
Detailed explanation

Hydrostatics- Buoyancy and metacentric height

detailed explanation of force of buoyancy, metacentric height,stability of floating body
unlimited numericals solved with updation weekly
including IOE , PU, KU, GATE, MIT, ANNA UNIVERSITY,UPSC EXAM SOLUTIONS
And much more

ORIFICES AND WEIRS

Complete IOE and GATE EXAM SOLUTION along with numerous Numericals from Fluid mechanics

Similar Question

This Chapter Flow-Past-Through-Submerged-Body consists of the following topics

Given: Military aircraft with M=8000 kg, lands on 350 km/hr and is slowed by a parachute with `A=10 m^2` area. Find

Estimate the time needed to slow to 200 km/hr.

Maximum deceleration rate.
Model the chute as an open hemisphere.

A kite has an effective area of `0.6 m^2` and mass 0.4 kg. It experience a drag of 15 N in a wind speed of 40 km/hr. Determine
tension in chord if it makes an angle of `45^0` with horizontal.

lift coefficient for kite
Consider density of air as 1.2 kg/`m^3`.

A 2000 kg aircraft is designed to carry a payload of 5000N when cruising at 300 km/hr. The effective wing area is `25 m^2`. Assuming a conventional airfoil, calculate the takeoff speed if the angle of attack of `10^0` is desired and the stall speed when landing.

A kite has an effective area of `0.6 m^2` and mass 0.4 kg. It experience a drag of 15 N in a wind speed of 40 km/hr. Determine the tension in the chord if it makes an angle of `45^0` with the horizontal. lift coefficient for the kite Consider the density of air as 1.2 kg/`m^3`.

Flow Past Through Submerged Body

Fluid-Mechanics