Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259129919
Author: John D. Anderson Jr.
Publisher: McGraw-Hill Education
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Chapter 1, Problem 1.17P
Consider the Space Shuttle during its atmospheric entry at the end of a mission in space. At the altitude where the Shuttle has slowed to Mach 9, the local heat transfer at a given point on the lower surface of the wing is
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Chapter 1 Solutions
Fundamentals of Aerodynamics
Ch. 1 - For most gases at standard or near standard...Ch. 1 - Starting with Equations (1.7),(1.8), and (1.11),...Ch. 1 - Consider an infinitely thin flat plate of chord c...Ch. 1 - Consider an infinitely thin flat plate with a 1 m...Ch. 1 - Consider an airfoil at 12 angle of attack. The...Ch. 1 - Consider an NACA 2412 airfoil (the meaning of the...Ch. 1 - The drag on the hull of a ship depends in part on...Ch. 1 - The shock waves on a vehicle in supersonic flight...Ch. 1 - Consider two different flows over geometrically...Ch. 1 - Consider a Lear jet flying at a velocity of 250...
Ch. 1 - A U-tube mercury manometer is used to measure the...Ch. 1 - The German Zeppeins of World War I were dirigibles...Ch. 1 - Consider a circular cylinder in a hypersonic flow,...Ch. 1 - Derive Archimedes principle using a body of...Ch. 1 - Consider a light, single-engine, propeller-driven...Ch. 1 - Consider a flat plate at zero angle of attack in a...Ch. 1 - Consider the Space Shuttle during its atmospheric...Ch. 1 - The purpose of this problem is to give you a feel...Ch. 1 - For the design of their gliders in 1900 and 1901,...Ch. 1 - Consider the existence of a forward-facing axial...
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- An air receiver carries a pressure of 3500 kPa absolute @ a temperature of 25 C. A fire occurs near the receiver which causes the temperature to rise to 80 C. Neglecting the increased volume of the receiver due to expansion, calculate the air pressure at this temperature.arrow_forwardAn airplane is flying at a velocity of 150 m/s at standard sea-level conditions. The temperature at a point on the wing is 270K. What is the pressure and velocity at that point? For air, C, = 1008- %3D kg Karrow_forwardAt 4000 m standard altitude, an aircraft is flying at 300 miles per hour. The air velocity relative to the top surface of the wing, at its maximum thickness, is 26% higher than the plane's velocity, as is normal. Calculate the absolute pressure at this location on the wing using Bernoulli's equation. Take elevation fluctuations and compressibility into account.arrow_forward
- A compressed air tank is designed to contain 50 standard cubic feet of air when Ölled to a gaugepressure of 200 atm at an ambient temperature of 70 F. Calculate the interior volume of thetank. One standard cubic foot of air occupies one cubic foot at standard temperature and pressure(T = 59 F and p = 2116 lb/ft2).arrow_forwardA spherical container fitted with a stirrer traps air with a volume equal to 5 cubic meters. The initial pressure of the air is 276 kPa and the initial temperature is 250 degrees Celsius. The wall of the container is thick enoughsuch that heat flow can be neglected. If the stirrer transfers 400 kJ of energy to the air, determine the final pressure (kPa) and temperature (degrees Celsius). At the top of your solution, write in bullet form all the assumptions you made in solving the problem.arrow_forwardDerive a formula for the bulk modulus of an ideal gas, with constant specific heats, and calculate it for steam at 300°C and 200 kPa. Compare your result to the steam tables.arrow_forward
- A vessel of volume 8.7m3 contains air and dry saturated steam (Psteam = 0.4bar, vsteam = 34.8m3/kg) at a total pressure of 0.06bar and temperature 29o. Calculate the mass of steam and Calculate the mass of air.arrow_forwardCompare the pressure of 30 kg of air in a vessel of temperature 300 K and volume 8 m3 by considering real gas and perfect gas.arrow_forwardIn a winter season in a certain country, you have to create steam at 100 centigrade at 1 atmosphere from a -10 centigrade snow. What energy will be consumed in kilojoules if the mass flow of steam is expected to be 1.5 kg/s? subject : Thermodynamicsarrow_forward
- You and Liza Soberano are in an aircraft flying steadily at 4,300m above sea level and you are about to experience your first sky dive with her. You jumped first but Liza, due to hesitation, jumped after few seconds. Supposed that in an instant, the barometric pressure at your elevation is 85.0 kPa and Liza is higher from you by 80om. Determine the barometric pressure at Liza's elevation assuming that pressure and temperature at sea level are 101.3 kPa and 25 deg.C respectively. Use lapse rate = 0.00650 K/m %3Darrow_forwardA tank of 10ft3 capacity is half filled with glycerin. The weight density of glycerin is 78.6 lbs/ft3 and its specific heat is 0.57 BTU/lb-°F. (a) How much heat is needed to raise the temperature of glycerin from 40°F to 70°F? (b) If the heat supplied to the glycerin is at a rate of 750 BTU/min, at what rate does its temperature rises?arrow_forwardWhat is the Mach Number of an air with a velocity of 250 m/s, at a temperature at 2800 meters?arrow_forward
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