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Correct Answer : Ablative surface
Explanation : The re – entry vehicles at hypersonic speed undergo viscous dissipation. This leads to rise in temperature within the boundary layer leading to excitation of the molecules causing dissociation or ionization. The surface of these vehicles are usually coated with ablative surfaces because of its high melting point and inert nature.
Correct Answer : Option (C) : Hypersonic flow over slender bodies
Explanation : Hypersonic similarity parameter K is an important governing parameter in order to study the hypersonic flow i.e. flow with Mach number greater than 5 over slender bodies. It is given by the product of free stream Mach number and flow deflection angle.
Correct Answer : Option (D) : Product of Mach number and slenderness ratio
Explaination : The product of Mach number and slenderness ratio along with gamma are the two parameters which appear in the non – dimensional equations. For a body that has same shape but have different scale ratio, if these parameters are same, the flow over them at hypersonic regime remain same. This is the physical meaning of the hypersonic similarity parameter.
K
γ
Correct Answer : Option (A) : Hypersonic similarity parameter K and γ
