Airplane Range in North Wind: Prove and Max Value

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SUMMARY

The discussion centers on the mathematical proof of an airplane's range in a north wind, specifically deriving the equation R(φ) = R(v² - n²) / [v(√(v² - n² sin²(φ))]. Participants explore the relationship between the airplane's speed (v), wind speed (n), and the angle (φ) relative to north. Key insights include the identification of the problem as a relative velocity issue and the importance of vector addition in calculating the airplane's effective speed during its journey. The maximum range and its directional attainment are also discussed, emphasizing the complexity of the problem.

PREREQUISITES
  • Understanding of vector addition and relative velocity
  • Familiarity with trigonometric functions and their applications in physics
  • Knowledge of Pythagorean theorem and its relevance in vector diagrams
  • Basic principles of flight mechanics and fuel consumption calculations
NEXT STEPS
  • Study vector addition in physics, focusing on relative velocity problems
  • Learn how to apply the Pythagorean theorem in real-world scenarios, particularly in aviation
  • Research the effects of wind on flight paths and fuel efficiency
  • Explore advanced trigonometry applications in physics, including sine and cosine laws
USEFUL FOR

Aerospace engineers, physics students, and anyone interested in understanding the dynamics of flight in varying wind conditions will benefit from this discussion.

  • #31
stop trying to work backwards from the answer …

work forwards! :smile:

and no, you don't need Pythagoras, just the sine rule and a bit of trig

(to make it easier to write, since C1 = C2, call them both θ, get an expression in φ θ and φ ± θ, and find cosθ in terms of n and v)

oh, and go to bed early tonight! :zzz:​
 
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  • #32
trumpsnuffler said:
hmmm, okay, would the time be calculated via pythagoras's theorem for the individual x and y components of v and n, for each journey repectively?

(n/v)sin(φ)..?

i'm a bit lost, i can see why the numerator is R(v+n)(v-n) and i can see that the v on the denominator comes from R/v, but i don't really get the last part, I'm still not sure where the pythagorian part of the denominator (√(v² - n²sin²φ)) and i guess I'm just clutching at straws a bit, trying to piece things together to make this last part.

God help me if a question like this comes up in my exam in a couple of days..

Never a diagram to be seen here.

The wind triangles are actually simple (as long as you remember you add vectors head-to-tail). I guess I should've made two separate ones also.
 

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  • #33
morning all, opted to get an early night in favour of an early rise!

okay, the above vector diagram's a bit misleading. on the return journey, the plane doesn't necessarily come fly off westwards to form a right angled triangle with Q v and n.

right the x and y components for the individual journeys are as follows

way there:

x component: v sinφ

y component: vcosφ - n

way back:

x component: v sinφ

y component vcosφ + n


although I'm guessing i must have done something wrong here as i have nothing involving θ
 
  • #34
hi trumpsnuffler! good morning! :smile:
trumpsnuffler said:
okay, the above vector diagram's a bit misleading. on the return journey, the plane doesn't necessarily come fly off westwards to form a right angled triangle with Q v and n.

yes, i don't like that diagram at all, but mostly because it puts the two wind vectors on different lines

flip that bottom triangle over, so that you have a nice double-triangle, with both parts to the left of the wind vectors :wink:
although I'm guessing i must have done something wrong here as i have nothing involving θ

what you've done is ok, just not very helpful …

you can always use components, but it'll be a lot easier (in this case) to use θ and the sine rule …

as i said, what is cosθ (n terms of n and v)? :smile:
 
  • #35
and with regards to the second part of the question 'find the maximum range and for which direction', would i have to go through the normal means of finding a maximum (i.e differentiating), and if so, differentiating with regards to what?

or do i just have to make n²sin²φ = 0, which would give the answer to be either φ = 0 or φ=180 (which would make sense in that to get the maximum range, the pilot has to fly either directly into the wind, or with the wind directly behind his back to eliminate any y component)?
 
  • #36
okay. as (n/v)sin(φ) = sin(θ)

(n/v)cos(φ) = cos(θ)

wasn't too sure if i could make this jump, but bearing in mind that the graphs of sin and cos are so similar, surely the above expression for cos(θ) holds to be true?
 
  • #37
trumpsnuffler said:
okay. as (n/v)sin(φ) = sin(θ)

(n/v)cos(φ) = cos(θ)

what?? not even close … sin is increasing and cos is decreasing!

use cos2 + sin2 = 1 :wink:
 
  • #38
oh wow. no idea why i didn't think of that.. :blushing:

okay. so cos² = 1 - sin²

cos² = 1 - sin²
= 1 - [(n/v)sin(φ)]²
= 1 - (n²/v²)sin²(φ)

therefore cosθ = √[1 - (n²/v²)sin²(φ)]

is the above expression the value of [t][/1] then? and [t][/2] = the same, but a positive (n²/v²)sin²(φ) instead?
 
  • #39
sorry, still getting to grips with using this forum. t1 and t2 were meant to be written in subscript..
 
  • #40
trumpsnuffler said:
therefore cosθ = √[1 - (n²/v²)sin²(φ)]

yup! :smile:

though to match the given answer, you might prefer to write it as (1/v)√[v² - n²sin²(φ)] :wink:
is the above expression the value of [t][/1] then?

no of course not, it's cosθ … why would that be t1?

(for subscripts, use the X2 icon just above the Reply box :wink:)
tiny-tim said:
if t1 and t2 are the times on the two legs, then t1 + t2 = R/v, so Q/R = Q/(vt1 + vt2) …

where can we read that fraction off the triangles? :smile:
 
  • #41
In the accompanying diagram air miles are proportional to time, of course. You might check out when b = 0. a = 0. and both a and b are sqr root of 2 times d.
 

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