Investigation of the Variation of Maximum Lift for a Pitching Airplane Model and Comparison with Flight Results
Author | : Paul W. Harper |
Publisher | : |
Total Pages | : 704 |
Release | : 1948 |
ISBN-10 | : STANFORD:36105024795820 |
ISBN-13 | : |
Rating | : 4/5 ( Downloads) |
Download or read book Investigation of the Variation of Maximum Lift for a Pitching Airplane Model and Comparison with Flight Results written by Paul W. Harper and published by . This book was released on 1948 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt: Apparatus was developed which utilized a pitching airplane model to determine maximum wing loads as a function of the rate of change of angle of attack. In order to evaluate the pitching-model technique, the maximum lift coefficient was determined as a function of the rate of change of angle of attack over a Mach number range from approximately 0.2 to 0.6 in wind-tunnel tests of a 1/20-scale model of a conventional single-engine fighter airplane and was conpared with existing flight data of this airplane. The wind-tunnel and flight results were found to be in good agreement.