Application of shock tubes to transonic airfoil testing at high Reynolds number

Application of shock tubes to transonic airfo ...
United States. National Aerona ...
Not in Library

My Reading Lists:

Create a new list

Check-In

×Close
Add an optional check-in date. Check-in dates are used to track yearly reading goals.
Today


Buy this book

Last edited by WorkBot
December 15, 2009 | History

Application of shock tubes to transonic airfoil testing at high Reynolds number

This edition doesn't have a description yet. Can you add one?

Buy this book

Edition Availability
Cover of: Application of shock tubes to transonic airfoil testing at high Reynolds number
Application of shock tubes to transonic airfoil testing at high Reynolds number
1978, National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Technical Information Service
in English

Add another edition?

Book Details


Edition Notes

Nov. 1978

Includes bibliographical references

Published in
[Washington], Springfield, Va
Series
NASA technical paper ; 1268

The Physical Object

Pagination
vi, 63 p. :
Number of pages
63

ID Numbers

Open Library
OL14932126M

Community Reviews (0)

Feedback?
No community reviews have been submitted for this work.

Lists

This work does not appear on any lists.

History

Download catalog record: RDF / JSON / OPDS | Wikipedia citation
December 15, 2009 Edited by WorkBot link works
September 16, 2008 Created by ImportBot Imported from Miami University of Ohio MARC record