The Evaluation of Propeller Aero-Acoustic Design Methods by Means of Scaled-Model Testing Employing Pressure Tapped Blades and Spinner
19th Congress ; 1994 ; Anaheim; CA
1994-01-01
13 pages
In 3 vols
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Online Contents | 1994
|RACER AERO-ACOUSTIC PROPELLER ANALYSIS AND DESIGN
British Library Conference Proceedings | 2019
|