EBK FUNDAMENTALS OF AERODYNAMICS
6th Edition
ISBN: 9781259681486
Author: Anderson
Publisher: MCGRAW HILL BOOK COMPANY
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Chapter 8, Problem 8.12P
Consider a flow with a pressure and temperature of
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1.1 Consider the fireclay brick wall of Example 1.1 that is
operating under different thermal conditions. The tem-
perature distribution, at an instant in time, is T(x) = a+
bx where a 1400 K and b = -1000 K/m. Determine
the heat fluxes, q", and heat rates, q, at x = 0 and x = L.
Do steady-state conditions exist?
2.4 To determine the effect of the temperature dependence
of the thermal conductivity on the temperature dis-
tribution in a solid, consider a material for which this
dependence may be represented as
k = k₁ + aT
where k, is a positive constant and a is a coefficient that
may be positive or negative. Sketch the steady-state
temperature distribution associated with heat transfer
in a plane wall for three cases corresponding to a > 0,
a = 0, and a < 0.
1.21 A one-dimensional plane wall is exposed to convective
and radiative conditions at x = 0. The ambient and sur-
rounding temperatures are T = 20°C and Tur = 40°C,
respectively. The convection heat transfer coefficient is
h=20 W/m² K, and the absorptivity of the exposed sur-
face is α=0.78. Determine the convective and radiative
heat fluxes to the wall at x = 0 if the wall surface tem-
perature is T, = 24°C. Assume the exposed wall surface
is gray, and the surroundings are large.
Chapter 8 Solutions
EBK FUNDAMENTALS OF AERODYNAMICS
Ch. 8 - Consider air at a temperature of 230 K. Calculate...Ch. 8 - The temperature in the reservoir of a supersonic...Ch. 8 - At a given point in a flow, T=300K,p=1.2atm, and...Ch. 8 - At a given point in a flow, T=700R,p=1.6atm, and...Ch. 8 - Consider the isentropic flow through a supersonic...Ch. 8 - Consider the isentropic flow over an airfoil. The...Ch. 8 - The flow just upstream of a normal shock wave is...Ch. 8 - The pressure upstream of a normal shock wave is 1...Ch. 8 - The entropy increase across a normal shock wave is...Ch. 8 - The how just upstream of a normal shock wave is...
Ch. 8 - Consider a flow with a pressure and temperature of...Ch. 8 - Consider a flow with a pressure and temperature of...Ch. 8 - Repeat Problems 8.11 and 8.12 using (incorrectly)...Ch. 8 - Derive the Rayleigh Pitot tube formula, Equation...Ch. 8 - On March 16, 1990, an Air Force SR-71 set a new...Ch. 8 - In the test section of a supersonic wind tunnel, a...Ch. 8 - When the Apollo command module returned to earth...Ch. 8 - The stagnation temperature on the Apollo vehicle...Ch. 8 - Prove that the total pressure is constant...
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- 1.12 You've experienced convection cooling if you've ever extended your hand out the window of a moving vehi- cle or into a flowing water stream. With the surface of your hand at a temperature of 30°C, determine the con- vection heat flux for (a) a vehicle speed of 40 km/h in air at -8°C with a convection coefficient of 40 W/m² K and (b) a velocity of 0.2 m/s in a water stream at 10°C with a convection coefficient of 900 W/m²K. Which condition would feel colder? Contrast these results with a heat flux of approximately 30 W/m² under normal room conditions.arrow_forwardPLEASE SOLVE STEP BY STEP WITHOUT ARTIFICIAL INTELLIGENCE OR CHATGPT SOLVE BY HAND STEP BY STEParrow_forward1. A 40 lb. force is applied at point E. There are pins at A, B, C, D, and F and a roller at A. a. Draw a FBD of member EFC showing all the known and unknown forces acting on it. b. Draw a FBD of member ABF showing all the known and unknown forces acting on it. c. Draw a FBD of member BCD showing all the known and unknown forces acting on it. d. Draw a FBD of the entire assembly ADE showing all the known and unknown forces acting on it. e. Determine the reactions at A and D. f. Determine the magnitude of the pin reaction at C. 40 lbs. B A 6 in. 4 in. D F -5 in.4 in 4.arrow_forward
- A crude oil of specific gravity0.85 flows upward at a volumetric rate of flow of 70litres per second through a vertical venturimeter,with an inlet diameter of 250 mm and a throat diameter of 150mm. The coefficient of discharge of venturimeter is 0.96. The vertical differences betwecen the pressure toppings is 350mm. i) Draw a well labeled diagram to represent the above in formation i) If the two pressure gauges are connected at the tapings such that they are positioned at the levels of their corresponding tapping points, determine the difference of readings in N/CM² of the two pressure gauges ii) If a mercury differential manometer is connected in place of pressure gauges, to the tappings such that the connecting tube up to mercury are filled with oil determine the difference in the level of mercury column.arrow_forwardCan you solve it analytically using laplace transforms and with Matlab code as well please. Thank Youarrow_forwardCan you solve it analytically using laplace transforms and with Matlab code as well please. Thank You.arrow_forward
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