__The propulsive power of the rocket is (where v‚Äö√á√Ö = Jet velocity, and v‚Äö√á√á = Aircraft velocity)__

Question

TuteeHUB · Accepted Answer

(v‚Äö√á√Ö - v‚Äö√á√á)¬¨‚â§/2g

TuteeHUB · Answer

(v‚Äö√á√Ö¬¨‚â§ -v‚Äö√á√á¬¨‚â§)/2g

TuteeHUB · Answer

(v‚Äö√á√Ö¬¨‚â§ -v‚Äö√á√á¬¨‚â§)/g

TuteeHUB · Answer

(v‚Äö√á√Ö - v‚Äö√á√á)¬¨‚â§/g

1.	__The propulsive power of the rocket is (where v‚Äö√á√Ö = Jet velocity, and v‚Äö√á√á = Aircraft velocity)__
A.	(v‚Äö√á√Ö¬¨‚â§ -v‚Äö√á√á¬¨‚â§)/2g
B.	(v‚Äö√á√Ö - v‚Äö√á√á)¬¨‚â§/2g
C.	(v‚Äö√á√Ö¬¨‚â§ -v‚Äö√á√á¬¨‚â§)/g
D.	(v‚Äö√á√Ö - v‚Äö√á√á)¬¨‚â§/g
Answer» B. (v‚Äö√á√Ö - v‚Äö√á√á)¬¨‚â§/2g

The propulsive power of the rocket is (where v‚Äö√á√Ö = Jet velocity, and v‚Äö√á√á = Aircraft velocity)