Application of shock tubes to transonic airfoil testing at high Reynolds number
197863 pages
National Aeronautics and Space Administration, Scientific and Technical Information Office·1 editions
Loading Description
Tags
NewBookshelves
0 readersNo users with this book on their shelves. Maybe you could be the first.
Threads
0 discussionsQuotes
0 quotesReviews
0 reviewsNo reviews yet. Add your review.
Lists
0 listsNo lists containing this book.