Static Longitudinal Characteristics At High Subsonic Speeds Of A Complete Airplane Model With A Highly Tapered Wing Having The 080 Chord Line Unswept And With Several Tail Configurations
Download Static Longitudinal Characteristics At High Subsonic Speeds Of A Complete Airplane Model With A Highly Tapered Wing Having The 080 Chord Line Unswept And With Several Tail Configurations full books in PDF, epub, and Kindle. Read online free Static Longitudinal Characteristics At High Subsonic Speeds Of A Complete Airplane Model With A Highly Tapered Wing Having The 080 Chord Line Unswept And With Several Tail Configurations ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configurations
Author | : Kenneth W. Goodson |
Publisher | : |
Total Pages | : 64 |
Release | : 1961 |
Genre | : Stability of airplanes, Longitudinal |
ISBN | : |
Download Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configurations Book in PDF, Epub and Kindle
An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The basic aspect-ratio-4.00 wing had a zero taper and an unswept 0.80 chord line. Several aspect-ratio modifications to the basic wing were made by clipping off portions of the wing tips. The complete model was tested with a chord-plane tail, a T-tail, and a biplane tail (combined T-tail and chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92. The data show that, when reduced to the same static margin, all the tail configurations tested on the model provided fairly good stability characteristics, the biplane tail giving the best overall characteristics as regards pitching-moment linearity. Changes in static margin at zero lift coefficient with Mach number were small for the model with these tails over the Mach number range investigated.
Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configurations Related Books
Pages: 64
Pages: 57
Pages: 102
Pages: 1
Pages: 388