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Assertion (A): In a supersonic nozzle, with sonic condition at the throat, any reduction of down stream pressure will not be felt at the inlet of the nozzle.Reason (R): The disturbance caused downstream of supersonic flowstravels at sonic velocity which cannot propagate upstream by Machcone.a)Both A and R are individually true and R is the correct explanation of Ab)Both A and R are individually true but R is not the correct explanation of Ac)A is true but R is falsed)A is false but R is trueCorrect answer is option 'A'. Can you explain this answer? for Mechanical Engineering 2024 is part of Mechanical Engineering preparation. The Question and answers have been prepared according to the Mechanical Engineering exam syllabus. Information about Assertion (A): In a supersonic nozzle, with sonic condition at the throat, any reduction of down stream pressure will not be felt at the inlet of the nozzle.Reason (R): The disturbance caused downstream of supersonic flowstravels at sonic velocity which cannot propagate upstream by Machcone.a)Both A and R are individually true and R is the correct explanation of Ab)Both A and R are individually true but R is not the correct explanation of Ac)A is true but R is falsed)A is false but R is trueCorrect answer is option 'A'. Can you explain this answer? covers all topics & solutions for Mechanical Engineering 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for Assertion (A): In a supersonic nozzle, with sonic condition at the throat, any reduction of down stream pressure will not be felt at the inlet of the nozzle.Reason (R): The disturbance caused downstream of supersonic flowstravels at sonic velocity which cannot propagate upstream by Machcone.a)Both A and R are individually true and R is the correct explanation of Ab)Both A and R are individually true but R is not the correct explanation of Ac)A is true but R is falsed)A is false but R is trueCorrect answer is option 'A'. Can you explain this answer?.

Solutions for Assertion (A): In a supersonic nozzle, with sonic condition at the throat, any reduction of down stream pressure will not be felt at the inlet of the nozzle.Reason (R): The disturbance caused downstream of supersonic flowstravels at sonic velocity which cannot propagate upstream by Machcone.a)Both A and R are individually true and R is the correct explanation of Ab)Both A and R are individually true but R is not the correct explanation of Ac)A is true but R is falsed)A is false but R is trueCorrect answer is option 'A'. Can you explain this answer? in English & in Hindi are available as part of our courses for Mechanical Engineering. Download more important topics, notes, lectures and mock test series for Mechanical Engineering Exam by signing up for free.

Here you can find the meaning of Assertion (A): In a supersonic nozzle, with sonic condition at the throat, any reduction of down stream pressure will not be felt at the inlet of the nozzle.Reason (R): The disturbance caused downstream of supersonic flowstravels at sonic velocity which cannot propagate upstream by Machcone.a)Both A and R are individually true and R is the correct explanation of Ab)Both A and R are individually true but R is not the correct explanation of Ac)A is true but R is falsed)A is false but R is trueCorrect answer is option 'A'. Can you explain this answer? defined & explained in the simplest way possible. Besides giving the explanation of Assertion (A): In a supersonic nozzle, with sonic condition at the throat, any reduction of down stream pressure will not be felt at the inlet of the nozzle.Reason (R): The disturbance caused downstream of supersonic flowstravels at sonic velocity which cannot propagate upstream by Machcone.a)Both A and R are individually true and R is the correct explanation of Ab)Both A and R are individually true but R is not the correct explanation of Ac)A is true but R is falsed)A is false but R is trueCorrect answer is option 'A'. Can you explain this answer?, a detailed solution for Assertion (A): In a supersonic nozzle, with sonic condition at the throat, any reduction of down stream pressure will not be felt at the inlet of the nozzle.Reason (R): The disturbance caused downstream of supersonic flowstravels at sonic velocity which cannot propagate upstream by Machcone.a)Both A and R are individually true and R is the correct explanation of Ab)Both A and R are individually true but R is not the correct explanation of Ac)A is true but R is falsed)A is false but R is trueCorrect answer is option 'A'. Can you explain this answer? has been provided alongside types of Assertion (A): In a supersonic nozzle, with sonic condition at the throat, any reduction of down stream pressure will not be felt at the inlet of the nozzle.Reason (R): The disturbance caused downstream of supersonic flowstravels at sonic velocity which cannot propagate upstream by Machcone.a)Both A and R are individually true and R is the correct explanation of Ab)Both A and R are individually true but R is not the correct explanation of Ac)A is true but R is falsed)A is false but R is trueCorrect answer is option 'A'. Can you explain this answer? theory, EduRev gives you an ample number of questions to practice Assertion (A): In a supersonic nozzle, with sonic condition at the throat, any reduction of down stream pressure will not be felt at the inlet of the nozzle.Reason (R): The disturbance caused downstream of supersonic flowstravels at sonic velocity which cannot propagate upstream by Machcone.a)Both A and R are individually true and R is the correct explanation of Ab)Both A and R are individually true but R is not the correct explanation of Ac)A is true but R is falsed)A is false but R is trueCorrect answer is option 'A'. Can you explain this answer? tests, examples and also practice Mechanical Engineering tests.