Effect of an Adjustable Supersonic Inlet on the Performance Up to Mach Number 2.0 of a J34 Turbojet Engine
Author | : Andrew Beke |
Publisher | : |
Total Pages | : 23 |
Release | : 1956 |
ISBN-10 | : OCLC:1109676512 |
ISBN-13 | : |
Rating | : 4/5 (12 Downloads) |
Book Synopsis Effect of an Adjustable Supersonic Inlet on the Performance Up to Mach Number 2.0 of a J34 Turbojet Engine by : Andrew Beke
Download or read book Effect of an Adjustable Supersonic Inlet on the Performance Up to Mach Number 2.0 of a J34 Turbojet Engine written by Andrew Beke and published by . This book was released on 1956 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: