The Effect of Air Density and Density Altitude on Landing Distance for Fixed Wing Aircraft | ||||
| The International Conference on Civil and Architecture Engineering | ||||
| Volume 15, Issue 15, May 2024, Page 1-1 PDF (245.52 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.1088/1755-1315/1396/1/012011 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| Abdel Latif G.A.L. Younes | ||||
| Civil Engineering Projects Sector, Military Production Company for Projects and Engineering Consultancy | ||||
| Abstract | ||||
| This thesis is concerned with studying the factors that effect on landing distance for fixed wing span aircrafts. These factors are divided related to types and characteristics of aircrafts, pilot's technique, runway surface conditions, weathering conditions, and other environmental factors. Among these factors that were analysed in details both Air Density and Density Altitude to determine the effect of each factor on landing distance for fixed wing span aircrafts, what is the impact ׳s percentage of factor? Also, to determine the extent impact of each on the other, and the factors that affect them. | ||||
| Keywords | ||||
| Air Density; Density Altitude; Atmospheric Pressure; Weather Systems; and Landing Distance | ||||
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