Free-flight simulation of the testing of supersonic inlet di
View on Open Library ↗

Free-flight simulation of the testing of supersonic inlet diffusers in a free jet wind tunnel with 50% area ratio in the Mach number range from 1.5 to 3

by

54 min read
Rate this book:
219 pages 1955

Buy This Book

As an Amazon Associate and Bookshop.org affiliate, BookOrb earns from qualifying purchases.

Know this book?

Help other readers discover this title by sharing your thoughts. Be the first to write a review.

Share Your Thoughts

Sign in to write a review.