Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259129919
Author: John D. Anderson Jr.
Publisher: McGraw-Hill Education
expand_more
expand_more
format_list_bulleted
Videos
Textbook Question
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
Expert Solution & Answer
Want to see the full answer?
Check out a sample textbook solution
Students have asked these similar questions
Determine the Mach Number of an airplane flying with a speed of 677 knots at a standard altitude of 39,344 ft.
Consider an airplane flying at a velocity of 250 m/s. Calculate its Mach number if it is flying at a standard altitude of (a) sea level, (b) 5 km, (c) 10 km.
What is the Mach number of a military jet traveling at 1250 km/h. If the atmospheric temperature is -32 degree Celsius.
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...
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 is flowing parallel to the plate at U∞=5 m/s and T∞=300 K over the flat plate of length L=0.1 m anddepth of 1 m into the paper, at the atmospheric pressure at the same temperature as the plate. Find;a) Boundary layer thickness at the point x = L of the plateb) Find the total resistance force acting on the two surfaces of the plate.c) The velocities in the hydrodynamic boundary layer are measured by a hot wire anomemeter. Thevelocity at x=0.1 m on the x component is measured as u=3 m/s. Find the distance from the plate and they component of velocity v.arrow_forwardA sled with two runners slides along a thin horizontal layer of water between the ice and the runners. The horizontal force that the water puts on the runners is equal to 2.4 lb when the sled's speed is 50 ft/s. The total area of both runners in contact with the water is 0.04 ft2, and the viscosity of the water is 3.5x10 lbs/ft2. Determine the thickness of the water layer under the runners. Assume a linear velocity distribution in the water layer.arrow_forwardThe door of a jet liner has dimension of 2.3m x 1.2m. if the inside pressure of cabin is 100kpaa , what force is exerted on the door when the plane flies at an altitude where the outside pressure is 15 kpaa.arrow_forward
- On a very cold day at the South Pole, the temperature of air is –60oF. Assuming that the air remains isothermal up to a 10,000 ft elevation and that the pressure at the sea level is 1 atm, calculate the pressure at 10,000 ft.arrow_forwardEvaluate the volume occupied by 8,968 kg of air at a gage pressure of 723 kPa and a temperature of 686 C . Calculate air density under the same conditions.arrow_forwardAn airliner is cruising at a velocity of 225 mps at an altitude of 14km in the standard atmosphere. Determine its Mach Number.arrow_forward
- The belt in the Ögure moves at steady velocity V and skims the top of a tank of oil having viscosity. (a) Develop and expression for the required belt drive power in terms of h, L, b, V , and . Recalthat, for steady motion, power is equal to force velocity.(b) What power is required if the belt moves at 5 m/s over SAE 50W oil ( = 0:86 kg/ms) withh = 2 cm, L = 2 m, and b = 0:5 marrow_forwardOver what range of temperature (in Kelvin) do you think it is reasonable to assume that the specific heat of air at constant pressure is constant for purposes of calculations in fluid mechanics? Justify your answerarrow_forwardA compressed air tank is designed to contain 50 standard cubic feet of air when filled to a gaugepressure of 200 atm at an ambient temperature of 70 F. Assume this is an air tank for scubadiving, and that the approximate shape of the tank is a cylinder with circular cross section. The interior volume of the tank is v=0.253 ft^3(a) If the interior length of the cylinder is 1 ft, what would be the inner diameter?(b) It is desired that the air tank be neutrally buoyant when empty. The density of aluminum is2700 kg/m3. If the tank is made of aluminum, what should be the wall thickness in order forit to be neutrally buoyant?arrow_forward
- Consider air at a temperature of 230 K. Calculate the speed of sound.arrow_forwardAn 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 aircraft wing is flying at an altitude of 25000ft above sea level. Calculate for the temperature, pressure and density on the wing at that altitude *arrow_forward
arrow_back_ios
SEE MORE QUESTIONS
arrow_forward_ios
Recommended textbooks for you
Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University Press
Mechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSON
Thermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEY
Mechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage Learning
Engineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY
Heat Transfer – Conduction, Convection and Radiation; Author: NG Science;https://www.youtube.com/watch?v=Me60Ti0E_rY;License: Standard youtube license