Answered: Find Temperature Ratio at Cruising…

Find Temperature Ratio at Cruising Altitude. Barometric Altimeter setting = 29.42 in.Hg Cruising Indicated Altitude = 9,500 ft Outside Air Temperature at altitude = 13.34 deg F 0.9120 0.8625

Refrigeration and Air Conditioning Technology (MindTap Course List)

8th Edition

ISBN:9781305578296

Author:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson

Publisher:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson

Chapter1: Heat, Temperature, And Pressure

Section: Chapter Questions

Problem 17RQ: Convert 22C to Fahrenheit.

See similar textbooks

Related questions

Q: The altimeter on a low-speed Cessna 172 reads 8,000 ft. By an independent measurement, the outside…

A: The true velocity of the airplane is 519.6 ft/sec.

Q: Pascal = (0.01 bar, 0.001 bar,0.0001 bar, 1O 100.000 bar)and T= 500 rankine what is the value in…

Q: H.W 5: A thermometer is used for the range of 200 to 400 F, and it is stated that its accuracy is…

Q: C1 (a). A lubricating oil having the dynamic viscosity of 0.052 poise and kinematic viscosity of…

A: Given Data: Dynamic viscosity=0.052 poise Kinematic viscosity=0.19 stokes

Q: 10. Gas from a bottle of compressed helium is used to inflate an inelastic flexible balloon,…

A: Work done by the balloon on the atmosphere,w=p*∆v P=760mmof Hg=1atm=1.01*10^5 Pa…

Q: The following date are provided for a pneumatic displacement gage shown in the figur Ambient…

A: Given: orifice diameter d1 = 0.75 mm outlet diameter d2 = 1.50 mm relationship for pressure ratio r,…

Q: Wind energy question #1 Q1) Wind at 1 standard atmospheric pressure and 15°C temperature has a…

A: Hi and thanks for the question. Since you have asked multiple questions, We will solve the first…

Q: 17. An automobile tire contains a certain volume of air at 30 psig and 70°F. The barometric pressure…

A: Given:P1=30 psig =206.843 KPaT1=70°F =294.261 KT2=160°F =344.261 K

Q: 15. Hydraulic oil with a Sg of 0.91 is pumped horizontally in a 2-in. I.D. distribution line at the…

Q: 6. A mierometer reading is used to indicate the displacement of the (a) boundary layer thickness (b)…

A: 6.

Q: Air with density of 1.225 kg/m^3 and viscosity of 1.789 x 10^-5 kg/m-s flows in a wind tunnel, the…

Q: Table 2 h Sea Level Vc knots 50 100 150 200 250 300 350 400 450 500 M h = 5,000 ft M - h = 10,000 ft…

A: Given: Vc is the calibrated air speed in knots. And→δ=PPo=PoPo=1 (because at sea level P=Po) And…

Q: 13. On a sea-level standard day, a pressure gage, moored below the surface of the ocean (SG =…

Q: Aerodynamics. Mach Number. Sub-So

A: given: Explain the following terms in your own words. Aerodynamics. Mach Number.…

Q: y aer. A Pitot tube is used to measure the air flow rate in a circular duct 8.5 m I.D. The "riowing…

Q: In Bourdon Gauge experiment, if the mass of the piston is 340 gr and mass of the platform is 173 gr,…

Q: How much time is required to inject a sample equal to 2.0% of the length of a 60 cm capillary if the…

A: Solution: Given Data: S=2%L=60 cmD=50×10-6 m∆P=2×104 Paμ=0.0010 kg/m-s

Q: 2. Complete the following if Patm = 100 kPa (yHg 13.6 YH,0) (Show your Solution) kPa (Gage)…

Q: The pilot of a Boeing 767 determines that a total of 22,300 kilograms of jet fuel is needed to fly…

Q: For the closed tank with Bourdan-tube gages tapped into it, what is the specific gravity of the oil…

Q: C1 (a). A lubricating oil having the dynamic viscosity of 0.058 poise and kinematic viscosity of…

A: Given data: The dynamic viscosity of the lubricating oil is μ=0.058 poise. The kinematic viscosity…

Q: A pitot-static tube to be used in 2n airplane for on-flight measurement was calibrated on ground by…

A: Given, Density, ρ= 1.20kg/m3Ambient pressure, Pa=70KPaAmbient density, ρa=0.91kg/m3Specific heat…

Q: In Bourdon Gauge experiment, if the mass of the piston is 340 gr and mass of the platform is 173 gr,…

A: Mass of piston = 340 gr Platform mass = 173 gr Absolute pressure error = 218.9 Pa

Q: A plate 0.05mm distant from a fixed plate moves at 1.15 m/s and required a force per unit area of…

A: As per the Bartleby rule, We’ll answer the first question since the exact one wasn’t specified.…

Q: 30°. 3. A container filled with water accelerates at 20 ft/s? up a plane inclined by a = pressure at…

Q: As shown in Fig. 1.12, a horizontal interface 0-0 exists between two immiscible liquids. The dynamic…

Q: A weather report indicates the barometric pressure is 29.75 in of mercury. What is the atmospheric…

A: Given, Brometric pressure ,P=29.75in of mercury.Now, we know that-1atm=14.7psiConverting psi into…

Q: If Reynolds number relate the inertial and viscous forces, which of the following relates the…

A: The correct option is (A) I.e., FROUDE NUMBER (Fr) In the dimensional and modal analysis, we have…

Q: Oil has a Kinematic viscosity of 1.5 x10 m2/S and a specific gravity of 0.80. What is its dynamic…

Q: P6.2 A 1:80 scale model of an aircraft was tested in air at 20C°moves with speed 40m/s a- What is…

A: Given, The velocity of the prototype in air, The kinematic viscosity of air, The kinematic…

Q: A certain gas at temperature equivalent to 24 degrees Celsius at 8 cu.m and 200 kPa is compressed to…

A: To find: The resulting pressure. Given: The initial pressure is Pi=200 kpa. The initial volume is…

Q: 10A plate 0.05mm distant from a fixed plate moves at 1.25 m/s and required a force per unit area of…

A: GIVEN DATA- 1(a) SHEAR STRESS =2.2N/m2 , U=1.25 m/s , y=0.05mm , Specific gravity of oil =0.7 1(b)…

Q: Air with density of 1.225 kg/m^3 and viscosity of 1.789 x 10^-5 kg/m-s flows in a wind tunnel, the…

Q: A certain gas at temperature equivalent to 24 degrees Celsius at 8 cu.m and 200 kPa is compressed to…

A: To find: The resulting pressure. Given: The initial pressure is P1=200 kPa. The initial temperature…

Q: An oil has a kinematic viscosity of 1.25 E-4 m 2 /s and aspecifi c gravity of 0.80. What is its…

A: Given data: Kinematic viscosity of the oil, ν = 1.25×10-4 m2/s. The specific gravity of the oil,…

Q: in Bourdon Gauge experiment, if the mass of the piston is 340 gr and mass of the platform is 173 gr,…

A: Given:mp=340 g =0.340 Kgmpl=173 g=0.173 KgA=244.8*10-6 m2Absolute pressure error,Pe=7398.3 Pa

Q: An engineer sets the pressure in a supply tank usinga very accurate manometer as a guide and then…

Q: The coefficient of friction for a flow through pipe with Reynold’s number 40000 is a. Need density,…

Q: Discharge, Q through a venturimeter depends on the following variable Inlet pipe diameter - D Throat…

A: π-Buckingham theorem: Given that variable Q is dependent upon given 5 variables, D, d, Δp, ρ, μ…

Q: The gage pressure of air in a pressurized water tank is measured simultaneously by both a pressure…

Q: 14. A certain industrial company buys gas at gage pressure of 500 KPa and 21° C and sells it at a…

A: 14. Option B is correct. 15. Option D is correct assuming the fluid to be air.

Q: The kinematic viscosity of liquid oil is 20 stoke and relative density = 0.85. Find the dynamic…

A: Given: kinematic viscosity of liquid = 20 stokes The relative density = 0.85

Q: A 300 mm by 150 mm Venturi meter (c = 0.985) carries 0.0566 m /s of water with a differential gage…

A: Given, Diameter of the pipe , D = 300 mm Diameter of the Venturi section , d = 150 mm Coefficient…

Q: Find the head lost due to friction in a pipe of radius 20 cm and length 50m, through which oil is…

A: In a Flow-through Pipes, losses are classified as 1) Major losses 2) Minor losses The losses are…

Q: Q) The velocity v (m/s) of air flowing past a flat surface is measured at several distances y(m)…

A: given; ⇒at y1=0.002m , velocity(v1)=0.287m/s⇒at y2=0.006m ,velocity(v2)=0.899m/s⇒stress…

Q: (a) A pitot-static probe shown in Figure 1 is a device that can be used to measure flowing liquid or…

A: stagnation pressure = static pressure + dynamic pressure

Q: 18. The Darcy-Weisbach equation is expressed as A. h=p/ B.h-/29 D.h= Kv/29) 19.A plot of the…

Q: Ql: A Pitot tube is used to measure the air flow rate in a circular duct 8.5 m I.D. The flowing air…

Question

Find Temperature Ratio at Cruising Altitude.

Barometric Altimeter setting = 29.42 in.Hg

Cruising Indicated Altitude = 9,500 ft

Outside Air Temperature at altitude = 13.34 deg F

0.9120

0.8625

0.2261

0.9312

Expert Solution

This question has been solved!

Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.

This is a popular solution!

SEE SOLUTION Check out a sample Q&A here

Step 1: Given Data

Step 2: From Table

Step 3: Calculation

Step 4: Result

Trending now

This is a popular solution!

Step by step

Solved in 4 steps

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.

Similar questions

Air flows over a flat plate at 38 m/s, 25°C and 1 atm pressure. The kinematic viscosity of air at 25°C is ν = 1.562 × 10−5 m2/s. If the critical Reynolds number is 5 × 105, at what distance from the leading edge of the plate would transition occur? (Round the final answer to three decimal places.)
The altimeter of a high speed business aircraft reads 3900 ft. A pitot tube situated on the fuselage reads 2620 psf. Calculate the aircraft's Mach number. Identify if Mach number is supersonic or subsonic? Round off answer to 2 decimal places.
Covert 15.14 poises to kinmetic viscosity in square feet per second if the liquid has a specific gravity of 0.964 Answer is in ft2/s
Find the reynolds number for an airplane wing, 4ft chord moving at 120 miles per hour through standard atmosphere. Round off nearest ten thousands
Calculate the individual uncertainties associated for measuring this velocity from the provide individual values given by the manufacture. Then determine the design stage instrument uncertainty. Which uncertainty (or which couple of uncertainties) is the most significant contributor? You attempt to determine the validity of a mass balance in your lab by repeatedly placing 100 g calibration weight on it. Fifteen readings were obtained with values of 101.2, 100.1, 99.8, 100.5, 101.1, 100, 100, 99.6, 101.5, 100.8, 100.9, 100.3, 99.8, 100.5, and 100.9 Estimate the bias error and the maximum precision error of the measurements
How to calculate permeability according to silica bead characxteristics without knowing pressure drop? silica diameter: 2.5mm Inlet mass flow rate: 0.3m^2/min Inlet Temperature: -10 degree C
An airfoil is being tested in a low-speed subsonic wind tunnel. The velocity of the flow in the test section is 76 ft/s, and the conditions are standard sea level. If the pressure at a point on the airfoil is 2,114 lb/ft2, what is the value of the pressure coefficient? (2 decimals) Use P=2116.8 psf and ρ=0.002377 slug/ft3 for SSLC pressure and density. Round off answer to the nearest hundredths, if the answer is negative include the negative sign.
Convert 67degree celcius to rankine
A thermometer is calibrated from 200degree centigrade to 300degree. the accuracy is specified as +-0.25%. Non Linearity is +-0.5% Hystersis is +-0.01% what is the maximum error
Convert 22C to Fahrenheit.
Qsafe = 187.586 MJ
Qn) A)What is thermocouple? Explain measurement system using Thermocouple with a neat schematic sketch. Draw the characteristics and write its different types with properties.