Question

Given a Density Ratio of 0.5328, what is the approximate Density Altitude?

Given a Density Ratio of 0.5328, what is the approximate Density Altitude?

Homework Answers

Answer #1

we haveat 0 ft we have sigma =1   at 20000 ft we have sigma = 0.5328at

Density Ratio of 0.5328 so....

15000 ft we have sigma = 0.6292for every ft higher than 15000 ft we have (0.6292−0.5328)/5000=1.928∗10−5(0.6292−0.5328)/5000=1.928∗10−5variation of σσtotal variation of σσ is 0.6292−0.5589=7.03∗10−20.6292−0.5589=7.03∗10−2which means a variation in altitude of 7.03∗10−2/1.928∗10−5=3646.37.03∗10−2/1.928∗10−5=3646.3 ft above 1500015000 ftthe density altitude is 15000+3646.3=18646.315000+3646.3=18646.3 ft

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
Aerodynamics 1- What is the effect of Weight, Density altitude, Wind and runway slope on landing...
Aerodynamics 1- What is the effect of Weight, Density altitude, Wind and runway slope on landing distance? 2- A 20% percent excess landing speed would cause a _____ percent increase in landing distance. 3- At sea level an aircraft has a minimum landing distance of 2000ft. What would be the minimum landing distance of the aircraft at 5000ft density altitude. 4- What is the effect on landing velocity and landing distance if there is a 15% increase of gross weight?(the...
Calculate the temperature and the density of atmospheric air at 3600 m altitude, when the field...
Calculate the temperature and the density of atmospheric air at 3600 m altitude, when the field of atmospheric pressures is given by the expression: p = p0 (1 - cz) ^(5.25) where z is the altitude,and p0 and c are constants p0 = 0.1x10^6Pa c = 0.021km^(-1). Consider the air as an ideal gas of molar mass M = 0.029kg/mol
The equation relating approximate barometric pressure (P, in torr) to altitude (h, in m) at room...
The equation relating approximate barometric pressure (P, in torr) to altitude (h, in m) at room temperature (T, °C) is ln P = 6.63 – (h/8000) Diethyl ether, CH3CH2OCH2CH3, a common organic solvent, has a normal boiling point of 34.6 °C (and thus a vapor pressure of 760 torr at 34.6 °C). At 25 °C, it has a vapor pressure of 532 torr. At what approximate altitude will diethyl ether boil at 25 °C? Where on Earth would it be...
At some altitude above the Earth’s surface, the density of air molecules is3.3×10^13 molecules/cm^3. At this...
At some altitude above the Earth’s surface, the density of air molecules is3.3×10^13 molecules/cm^3. At this altitude, the temperature is −44°C. What is the mean free path of air molecules at this altitude? Assume a molecular diameter of 2.1×10^-8??. What is the pressure at this altitude?
At an altitude of 11000 m (a typical cruising altitude for a jet airliner), the air...
At an altitude of 11000 m (a typical cruising altitude for a jet airliner), the air temperature is -54.0 ∘C and the air density is 0.410 kg/m3 . What is the pressure of the atmosphere at that altitude? (Note: The temperature at this altitude is not the same as at the surface of the earth, so the equation P=P0exp(−MgyRT) doesn't apply.)
Construct a triangle, given side BC, ∠A and length of the altitude from vertex A.
Construct a triangle, given side BC, ∠A and length of the altitude from vertex A.
Discussion 1. What will be the approximate value of degree of saturation at OMC? 2. How...
Discussion 1. What will be the approximate value of degree of saturation at OMC? 2. How does the amount of compaction affect the maximum dry density and optimum moisture content of a given soil? 3. What is the use of Proctor’s needle? How is it used for compaction control in a field ?
a) Determine the variation of Earth's atmosphere in function of altitude (y), above the sea level,...
a) Determine the variation of Earth's atmosphere in function of altitude (y), above the sea level, assuming a constant geavity (g) and that the density of the air is proportional to the pressure. b) At what altitude the pressure of the air is the same as halve the pressure at sea level? c) Graph pressure against altitude.
An aircraft flies at an altitude of 30,000 feet. Determine the air temperature (in [K]), air...
An aircraft flies at an altitude of 30,000 feet. Determine the air temperature (in [K]), air pressure (in [Pa]) and air density (in [kg/m3]) at this altitude, according to the standard atmosphere.
A. At what altitude above the Earth's surface would a satellite have to be for it’s...
A. At what altitude above the Earth's surface would a satellite have to be for it’s orbital period to be equal to 24 hours? Assume the satellite is in a circular orbit. Assume a spherical, uniform density for the Earth. The Earth's mass 5.98 x 10 raised to 24kg. The Earth's radius is 6380 km B. Why would a satellite in such an orbit be a useful thing?
ADVERTISEMENT
Need Online Homework Help?

Get Answers For Free
Most questions answered within 1 hours.

Ask a Question
ADVERTISEMENT