Related InterviewSolutions

• For a steady, inviscid, adiabatic flow of a gas, the total temperate is constant along the flow.(a) True always(b) False always(c) True only for calorically perfect gas(d) False only for calorically perfect gasThe question was asked in an international level competition.Asked question is from Definition of Total Stagnation Conditions in division Compressible Flow – Preliminary Aspects of Aerodynamics
• Specific heat for gas is almost constant in the case of_______(a) Space vehicle(b) High-temperature flow(c) Air in a desert(d) Chemically reacting flow at high- speedsThis question was posed to me in semester exam.This is a very interesting question from A Brief Review of Thermodynamics topic in chapter Compressible Flow – Preliminary Aspects of Aerodynamics
• Select the incorrect statement if all the streamlines of the steady, inviscid, adiabatic flow originate from a common uniform freestream.(a) Stagnation enthalpy is same for each streamline(b) h0 is constant along the entire flow(c) h0 is not equal to the freestream value(d) h + V^2 = h0 is energy equation per unit massI have been asked this question by my school teacher while I was bunking the class.The question is from Definition of Total Stagnation Conditions in section Compressible Flow – Preliminary Aspects of Aerodynamics
• Select the incompressible flow out of the following.(a) High speed gaseous flow(b) M=5(c) M=3(d) Liquid flowI had been asked this question in an interview.This intriguing question originated from Definition of Compressibility topic in section Compressible Flow – Preliminary Aspects of Aerodynamics
• τT and τS are precise thermodynamic properties of the gas and the values can be obtained easily.(a) True always(b) False alwaysI had been asked this question in an internship interview.Question is from Definition of Compressibility in chapter Compressible Flow – Preliminary Aspects of Aerodynamics
• The total enthalpy in a general flow at point 1 is H1 and at point 2, which is downstream, is H2. Then __________(a) H1>H2 always(b) H2>H1 always(c) H1=H2 for general flow(d) H1=H2 for adiabatic flowThe question was posed to me by my school teacher while I was bunking the class.I want to ask this question from Definition of Total Stagnation Conditions in portion Compressible Flow – Preliminary Aspects of Aerodynamics
• An isentropic process is restrictive and is not feasible in real life.(a) False(b) TrueThis question was addressed to me in quiz.This intriguing question comes from A Brief Review of Thermodynamics in portion Compressible Flow – Preliminary Aspects of Aerodynamics
• Which is the process in which no heat exchange is there between system and surroundings and in which no dissipative phenomena occur?(a) Adiabatic process(b) Reversible process(c) Isentropic process(d) WorkThe question was posed to me in final exam.My query is from A Brief Review of Thermodynamics topic in division Compressible Flow – Preliminary Aspects of Aerodynamics
• The stagnation pressure can be visualized as the pressure we feel when we ride along the gas molecules at the local flow velocity.(a) False(b) TrueI got this question in an interview for job.This intriguing question comes from Definition of Total Stagnation Conditions topic in section Compressible Flow – Preliminary Aspects of Aerodynamics
• The quantity at a point in a subsonic flow where the element is speeded up to sonic velocity adiabatically is defined as_____(a) Static local temperature, T(b) Stagnation local temperature, T°(c) T*(d) Standard temperatureI got this question in an internship interview.My question comes from Definition of Total Stagnation Conditions in portion Compressible Flow – Preliminary Aspects of Aerodynamics