My WebLink
|
Help
|
About
|
Sign Out
Home
FAA Regulations
Ramsey
>
Public
>
Dissolved Boards/Commissions/Committees
>
Airport Commission
>
Miscellaneous
>
FAA Regulations
Metadata
Thumbnails
Annotations
Entry Properties
Last modified
7/29/2024 3:58:21 PM
Creation date
5/12/2010 11:45:08 AM
Metadata
Fields
Template:
Miscellaneous
Jump to thumbnail
< previous set
next set >
There are no annotations on this page.
Document management portal powered by Laserfiche WebLink 9 © 1998-2015
Laserfiche.
All rights reserved.
/
572
PDF
Print
Pages to print
Enter page numbers and/or page ranges separated by commas. For example, 1,3,5-12.
After downloading, print the document using a PDF reader (e.g. Adobe Reader).
View images
View plain text
6/24/75 AC 150/5300-48 <br />CHAPTER 3. WIND ANALYSIS AND RUNWAY ORIENTATION <br />8. GENERAL. <br />a. The configuration of the airport is determined by the number and <br />orientation of the runways. One of the primary factors influencing <br />runway orientation is wind. Ideally the runway should be aligned <br />with the prevailing winds. Wind conditions affect all airplanes, <br />the smallest to the largest, in varying degrees. Generally, the <br />smaller the airplane, the more it is affected by wind, particularly <br />crosswind components. Crosswinds are often a contributing factor <br />in small airplane accidents. In some cases, construction of two <br />runways may be necessary to give the desired wind coverage. <br />b. Airport planners and designers should, therefore, make an accurate <br />analysis of wind to determine the orientation and number of runways. <br />The proper application of the results of this analysis will add <br />substantially to the safety and usefulness of the airport. Appendix <br />3 provides information on wind data for the purpose of airport plan- <br />ning and design, and the following paragraphs give procedures in its <br />application to runway orientation concepts. <br />9. CROSSWINDS. <br />a. A crosswind component of wind direction and velocity is the resultant <br />vector which acts at a right angle to the runway. It is equal to the <br />wind speed multiplied by the trigonometric sine of the angle between <br />the wind direction and the runway direction. Normally, these wind <br />vector triangles are solved graphically. An example is shown in <br />Figure 3-1. From this diagram, one can also ascertain the headwind <br />and tailwind component of combinations of wind velocities and direc- <br />tions. <br />b. Study and analysis of different combinations of velocities and <br />directions, having an 11.4-mile-per-hour (mph) (9.9 knots) cross- <br />wind component, have found that different combinations produce <br />similar adverse effects on the control handling characteristics of <br />airplanes. Considering this and the method of repotting wind data, <br />the 12-mph or 10.5-knot speed was selected as a reasonable and <br />convenient figure upon which to base runway orientation. <br />11). ORIENTATION AND COVERAGE. The most desirable runway orientation based <br />on wind is the one which has the largest wind coverage and minimum <br />crosswind components. <br />Chap 3 <br />Par 8 <br />Page 7 <br />
The URL can be used to link to this page
Your browser does not support the video tag.