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Aeronautical Engineering/wind tunnel corrections

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Question
what are the calculations used in solid blockage,wake blockage,tare and interference corrections,stream line curvature?

Answer
Jai
Books have been written on this subject, which is much too broad for me to answer in detail.  I refer you to the book:

Pope A and Rae WH. Low-Speed Wind Tunnel Testing, John Wiley, New York, 1984.

Wind tunnel walls produce numerous effects on wind tunnel models that are not found in flight.  Rae and Pope list nine effects in the beginning of chapter 6.  The so-called solid blockage causes an increase in dynamic pressure, which affects all the aerodynamic forces.  In addition, wake blockage primarily affects drag and requires a special correction to drag.  Other factors alter the model angle of attack, which primarily affects lift.  So, to answer your question, engineers calculate different corrections for lift, drag, and moments except for the dynamic pressure correction which affects all forces equally.  The calculations are summarized in the book.

You can also find information by googling wind tunnel corrections.
Paul

Aeronautical Engineering

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Paul Soderman

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Aeronautics, Fluid Mechanics, Aeroacoustics, Noise Control, Muffler Design, Wind Tunnel Research.... I know nothing about India - do not ask about schools, jobs, application requirements, career choices, etc. for India. Please, no text message verbiage; I prefer full words in full sentences. Thanks.

Experience

38 years as research engineer at NASA

Publications
AIAA, NASA

Education/Credentials
B.S. and M.S. Aeronautical Engineering - U. of Washington Graduate work Standford U.

Awards and Honors
AIAA Associate Fellow (American Institute of Aeronautics and Astronautics)

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