CH10: Similarity Rules Flashcards

1
Q

What dimensionless terms characterize the Cp in two dimensional axially symmetric flow of a perfect gas.

A

Cp = f(x/c, M, gamma, t/c)

GD, Roshko, Pg. 252

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2
Q

What is the main difference between similarity considerations and dimensional analysis?

A

Dimensional analysis simply lists the dimensionless parameters that are involved, whereas similarity analysis shows how to group these dimensionless quantities in such a way as to reduce the number of independent variables.

GD, Roshko, Pg. 253

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3
Q

True or False
For linearized equations, it is essential to make a study of similarity in order to gain useful physical results.

A

False

GD, Roshko, Pg. 253

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4
Q

What similarity rules exist for two-dimensional linearized flow?

A

Two members of a family of shapes characterized by the thickness ratios tau1 and tau2 have pressure distributions given by coefficients cp1 and cp2.

GD, Roshko, Pg. 255

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5
Q

The hypersonic similarity parameter is defined as K = _____.

A

M_infinity * Tau

Where Tau = is the body thickness ratio.

GD, Roshko, Pg. 265

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6
Q

True or False
At very high Mach numbers, the mock angle may be of the same order or less than the maximum deflection angle of the body.

A

True.

GD, Roshko, Pg. 265

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7
Q

True or False
For large values of the hypersonic parameter, the difference between beta (the shock angle) and mu (the Mach angle) is not important.

A

False

GD, Roshko, Pg. 265

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8
Q

In the transonic case, the ______ extend to the field is large and changes________ the direction of the flow are of main importance.

A

lateral
along

GD, Roshko, Pg. 265

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9
Q

In the hypersonic regime, the flow field is very ________ , since the shockwaves lie close to the body, and the changes________ To the direction of flow are the most important ones.

A

narrow
normal

GD, Roshko, Pg. 265

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10
Q

True or False
In hypersonic flow it is generally not possible to assume irrotational flow, with a corresponding velocity potential.

A

True.

GD, Roshko, Pg. 265

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