Normal view MARC view ISBD view

Simplified fourwall interference assessment procedure for airfoil data obtained in the langley 0.3-meter transonic cryogenic tunnel

Simplified fourwall interference assessment procedure for airfoil data obtained in the langley 0.3-meter transonic cryogenic tunnel - - Washington, D.C. National Aeronautics and Space Adminstration 1987 - 60 p. - NASA CR 4042 : 1987 .

ISBN:

Subjects--Topical Terms:

Airfoil testing, Wind tunnel testing, Wall interference

Universal Decimal Class. No.: LNASA CR 4042 : 1987

Print
Add to your cart (remove)
More searches

Search for this title in:
Other Libraries (WorldCat) Other Databases (Google Scholar) Online Stores (Bookfinder.com) Open Library (openlibrary.org)