What is the marine layer density of the city of Richmond CA?
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This area stretches 20 miles from the Richmond area through Oakland to San Leandro. Its western boundary is defined by the San Francisco Bay and its eastern boundary by the Oakland-Berkeley Hills. The Oakland-Berkeley Hills are a significant barrier to air flow having an approximate ridge line height of 1500 feet. The most densely populated area of the region is that strip of land between the bay and the 500 foot elevation, where most people live, drive and work. It is a narrow strip of land averaging about 4 miles in width, with a 2 mile minimum in the Berkeley and southern Richmond areas and an 8 mile maximum at points in the San Leandro and Oakland areas. This area is home to an  international  airport, major chemical, petroleum, shipping and other industrial operations, a large university, a major military facility (in the process of being decommissioned) and over 3/4 of a million people.
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There should be estimates with the Marin County Department of Health.  This is their website: http://www.co.marin.ca.us/depts/HH/main/index.cfm\n\nAccording to the state of California Marin County has:\n1,556 Total Cases\n643 Living Cases\n913 Number of Deceased\n58.7% Percent of total cases deceased.
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density of pure water is 62.4 lbs/sq ft.\n\nSo, load = dAgh\n\nor A = 40000/(62.4*5*32) = 4.01 sq ft.
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Go this site and scroll down through, you will find all of the information you need.\n\nhttp://www.cia.gov/cia/publications/factbook/geos/ca.html
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Greetings from San Rafael (in beautiful Marin).\n\nWe're on the north side of the Golden Gate Bridge from San Francisco.  We have the SF bay to our East, and the Pacific Ocean to the West with some gorgeous coastline, and Mt. Tamalpais (we call it Tam) in the center of the county (quite a great mtn. bike ride).
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Density and phase 0.626 g/cm3, liquid
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With a Altimeter,zero at sea level.Then go to each city.You'll get your answers.Or you could google for your answer.
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The density of air, ρ (Greek: rho) (air density), is the mass per unit volume of Earth's atmosphere, and is a useful value in aeronautics. In the SI system it is measured as the number of kilograms of air in a cubic meter (kg/m3). At sea level and at 20 °C dry air has a density of approximately 1.2 kg/m3. varying with pressure and temperature. Air density and air pressure decrease with increasing altitude.\n\nThe formula for the density of air is given by:\n\n P=p/R*T\nwhere ρ is the air density, p is pressure, R is the gas constant, and T is temperature.\n\nThe individual gas constant R for dry air is:\n\n R( dry air )=287.05J/kg*K\nTherefore:\n\nAt standard temperature and pressure (0 °C and 101.325 kPa), dry air has a density of ρSTP = 1.293 kg/m3. \nAt standard ambient temperature and pressure (25 °C and 100 kPa) dry air has a density of ρSATP = 1.168 kg/m3. \n[edit]\nEffect of water vapor\nFor moist air, the partial pressure of the water vapor must be considered as well. In this case, the density of the air is the sum of the density of the dry air and the density of the water vapor:\nP=pdry air /Rdry air*T+p water vapour/R water vapour*T\n \nThe gas constant for water vapor is:\nR water vapour=461.495 J/kg*K\n \nEffects of altitude\nTo calculate the density of air as a function of altitude, one requires additional parameters. They are listed below, along with their values according to the International Standard Atmosphere, using the universal gas constant instead of the specific one:\n\nsea level atmospheric pressure p0 = 101325 Pa = 1013.25 mbar or hPa = 101.325 kPa (= 101325 kg/(m*s2)) \nsea level standard temperature T0 = 288.15 K \nEarth-surface gravitational acceleration g = 9.80665 m/s2. \ndry adiabatic lapse rate L = −0.0065 K/m \nuniversal gas constant R = 8.31447 J/(mol·K) \nmolecular weight of dry air M = 0.0289644 kg/mol \nTemperature at altitude h metres above sea level is given by the following formula (only valid below the tropopause):\n\n T=To+L*H\nImportance of temperature\nThe below table demonstrates that the properties of air change significantly with temperature.\n\nTable — speed of sound in air c, density of air ρ, acoustic impedance Z vs. temperature °C\n\nImpact of temperature \n°C c in m/s ρ in kg/m³ Z in Pa·s/m \n- 10 325.4 1.341 436.5 \n- 5 328.5 1.316 432.4 \n0 331.5 1.293 428.3 \n+ 5 334.5 1.269 424.5 \n+ 10 337.5 1.247 420.7 \n+ 15 340.5 1.225 417.0 \n+ 20 343.4 1.204 413.5 \n+ 25 346.3 1.184 410.0 \n+ 30 349.2 1.164 406.6
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125% the density of water.
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Hi, \n\nIf you mean east bay...\n\nBerkeley... California... You Have Me!!\n\nCheers!!\n\n(ONLY JOKING BY THE WAY, DUDE!!)
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Uh, I don't know the density, BUT it has as many people as New York City.  (around 17,000,000) \nI found this out from Claudia, an Austrian girl who studied in New York.
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try the Santa Monica bay. just spear the floaters!
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Try this:\nhttp://www.gop.com/States/StateDetails.aspx?state=CA
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Irvine Ca - From $40 to $1090 a month.\n\nRegards
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http://www.sunnybrook.on.ca/~yaffe/research/density/density.html
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Staten Island is one of the five borough's of New York City. The Island is 13.9 miles long, and 7.3 miles wide.
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Salton Sea.  It's in either Riverside or San Diego County.