In order to compute the airport reference temperature and the standard temperature with respect to elevation, the monthly mean of average daily temperature and the monthly mean of the maximum daily temperature of the hottest month of the year is found to be 32° C and 41.5° C respectively. The airport reference temperature is:

In order to compute the airport reference temperature and the standard temperature with respect to elevation, the monthly mean of average daily temperature and the monthly mean of the maximum daily temperature of the hottest month of the year is found to be 32° C and 41.5° C respectively. The airport reference temperature is:

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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Q2; Find the airport temperature knowing that: the airport elevation is 1500 ft above the sea level, the effective runway gradient is 0.16, the planned runway length is 4000 ft & the basic runway length is 3200 ft.
HELP ME ASAP PLS Consider: Air Pressure at 1500m, in kPa Round to two (2) decimal places 7. Estimate the vapor pressure, air pressure, relative humidity, and air density at a height of 1800 m into the atmosphere. The total pressure is 101 kPa, air temperature is 25°C and the dew point temperature is 15°C near the ground, the lapse rate 7.5°C/km, which is constant for both air temperature and dew point temperature. The gas constant R is 287 J/kg-K and constant with respect to altitude.
Problem 1: calculated the monthly average of the following climate ciements for the period (2007-2016)
Subject:-( Transportation planning and engineering )
An airport is to be constructed at a site 190m above mean sea level and on a level ground. The runway length required under standard atmospheric condition at sea level for landing is considered as 2100m and for take-off as 1600m respectively. Determine the actual runway length to be provided at this airport site. Airport reference temperature may be considered as 21-degree C.
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Subject: ( Transportation planning and engineering )
A weatherman carried an aneroid barometer from the ground floor to his office atop a certain building. On the level ground, the barometer reads 40 in.Hg.A; topside read 29in.Hg.A. The average atmospheric air density was 0.08 lb/cu.ft. Estimate the height of the building.
On the mountain in Kalinga ,a mountain biker carried an aneroid barometer in his bike from base to top. On the ground level, the barometer read 35.12 in. Hg absolute; topside it read 26.807 in. hg absolute. Supposing that the average atmospheric air density was 0.075 lb/ft^3, estimate the height and slope distance of the mountain if the average slope angle is 32 degrees .
Aerodynamic Method
#1 The maximum and minimum temperature recorded at a Lake is 18°C and 15°C in February. The mean air temperature (T), pan evaporation (Ep), wind speed (uz), relative humidity (RH), and net radiation (Rn) in a nearby weather station were found to be 23°C, 15 mm/day, 23 m/s, 47%, 20.54 MJ/m²/day, respectively. Estimate Lake evaporation (mm/day) using: (a) Pan Evaporation method, (b) Aerodynamic method, (c) Energy balance method, and (d) Penman method of combined aerodynamic and energy balance algorithm. Data you may need: 19.65 T Saturation vapor pressure, es = 611 e 273+T) where T is temperature in °C and es in Pa (You can also use table to read off the value of e, from internet or textbook (Table 2.9 or Appendix A) Assume, Pan Coefficient = 0.7 Bulk evaporation coefficient, CE = 1.3×10-3 Vapor pressure at elevation Z; ez = RH*es Atmospheric pressure at sea level = 101.3 kPa Density of air = 1.19 kg/m³ and for water = 1000 kg/m³ Bowen ratio = 0.1 Latent heat of vaporization (2) = 2.447…
HELP ME ASAP PLS Consider: Vapor Pressure at 1500m, in Pa Round to the nearest whole number 8. Estimate the vapor pressure, air pressure, relative humidity, and air density at a height of 1800 m into the atmosphere. The total pressure is 101 kPa, air temperature is 25°C and the dew point temperature is 15°C near the ground, the lapse rate 7.5°C/km, which is constant for both air temperature and dew point temperature. The gas constant R is 287 J/kg-K and constant with respect to altitude.|