Solving For Unknown Vector Components

Click For Summary

Homework Help Overview

The discussion revolves around determining the original speed of an aircraft prior to encountering wind, given its resulting speed, original heading, wind speed, wind direction, and final heading. The subject area includes vector components and their interactions in a physics context.

Discussion Character

  • Exploratory, Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • Participants explore the relationship between the aircraft's initial and final velocities, the wind's influence, and the use of vector components. Questions arise regarding whether to eliminate or invert wind components, and how to set up equations based on the new coordinate system. Some participants attempt to rearrange equations to isolate the initial velocity.

Discussion Status

Participants are actively engaging with the problem, offering various approaches and questioning assumptions about the setup. There is no explicit consensus, but some guidance has been provided on how to manipulate the equations to find the unknowns.

Contextual Notes

Participants note the need to clarify what is required in the original problem, specifically regarding the final aircraft velocity and angular displacement. There is also mention of potential miscalculations in determining the initial speed.

Badmachine
Messages
13
Reaction score
0

Homework Statement



Is it possible to determine aircraft speed prior to contact with noted wind, if resulting aircraft speed, original aircraft heading, wind speed and wind direction and final aircraft heading are known?

Homework Equations



P (plane): Bearing 241° (traveling approximately southwest) @ "X" f/s.
W (wind): Traveling south @ 32 f/s.

Plane and wind components represented by ordered pairs:

P = ["X" f/s cos(241°), "X" f/s sin(241°)] = ?, ?
W = [-32 f/s cos(90°), -32 f/s sin(90°)] = 0, -32

? + 0 = ?
? + (-32) = ?

||P + W|| = ?² + ?² = ?^(1/2) = 710 f/s

tan −1(?/?) = 62.24° + 180° = 242.24°

Displacement = 242.24° - 241° = 1.24°

The Attempt at a Solution

 
Last edited:
Physics news on Phys.org
Select a co-ordinate axis so that final direction of the plane (Pf) is along -x-axis.
Let the angle of the initial direction of the plane (Pi) with he new x-axis be α.
Let the angle of the direction of the wind (W) with he new x-axis be β. From the given data you can find β.
Now sum of the x-components of Pi and W is equal to Pf.
And y component of Pi is equal and opposite to y-component of W.
Write the equations and solve.
 
Does the solution require eliminating the wind components or inverting the wind compinent's values?
 
Badmachine said:
Does the solution require eliminating the wind components or inverting the wind compinent's values?
The two equations become
(Pi)x + (W)x = (Pf) ...(1)

(Pi)y + (W)y = 0...(2)
Rearrange the equations.

(Pi)x = - (W)x + (Pf) ...(3)

(Pi)y = -(W)y ...(4)
Square eq. 3 and 4 and add to get (Pi)
 
Thanks rl. Let's see if I am following you correctly.

(Pi)x = - (W)x + (Pf)

(Pi)y = -(W)y



(Pi)x = - (0)x + (P[710 f/s]f)

(Pi)y = -(32)y

710² + 32² = 505,124^(1/2) = 710.72

Apparently I'm performing the calculations incorrectly, as Pi = 683 f/s (value omitted in original post).

Original problem:

P (plane): Bearing 241° (traveling approximately southwest) @ 683 f/s (465 mph); W (wind): traveling south @ 32 f/s (22 mph)

[683 f/s cos(241°), 683 f/s sin(241°)] = -331, -597
[-32 f/s cos(90°), -32 f/s sin(90°)] = 0, -32

-331 + 0 = -331
-597 + (-32) = -629

||P + W|| = 331² + 629² = 505, 2021/2 = 710 f/s

tan −1(629/331) = 62.24° + 180° = 242.24°

Displacement = 242.24° - 241° = 1.24°
 
Last edited:
What is required in the original problem?
For example, if the want to cross a river and reach the opposite bank, you have to row in the upstream direction. Similarly which velocity is given in the problem?
 
rl.bhat said:
What is required in the original problem?

To determine the final aircraft velocity (Pf) and angular aircraft displacement from original heading, after application of a given wind.

Had hoped to learn how to "reverse engineer" for the original aircraft speed (Pi) or even heading simply based on other knowns.
 
OK. It can be done in the following way. Refer my post#2 and #4
Pi*cosα + W*cosβ = Pf Or
Pi*cosα = Pf - W*cosβ
Pi*sinα = W*sinβ
Pi^2 = ( Pf - W*cosβ )^2 + (W*sinβ)^2
In the given problem, if the velocity of plane is Pf, then β = 270degrees - 241 degrees.
So using the above equation you can find Pi.
 
Thanks rl.

Perhaps I miscalculated somehwere, but at this stage I arrive at Pi = 649 f/s (as opposed to 683 f/s)

β = 270degrees - 241 degrees = 29
Pi^2 = ( Pf - W*cosβ )^2 + (W*sinβ)^2
Pi^2 = [710 - (-32)*cos29]^2 + [(-32)*sin29)]^2
421,400 = 421,159 + 241
649 f/s
 

Similar threads

  • · Replies 2 ·
Replies
2
Views
3K
Replies
11
Views
2K
Replies
3
Views
2K
  • · Replies 6 ·
Replies
6
Views
2K
  • · Replies 9 ·
Replies
9
Views
2K
  • · Replies 29 ·
Replies
29
Views
3K
  • · Replies 5 ·
Replies
5
Views
2K
Replies
3
Views
3K
  • · Replies 2 ·
Replies
2
Views
2K
  • · Replies 1 ·
Replies
1
Views
1K