Wind Tunnel Investigation Of The Aerodynamic Characteristics In Pitch And Sideslip At High Subsonic Speeds Of A Wing Fuselage Combination Having A Triangular Wing Of Aspect Ratio 4 PDF Download
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| Author | : Paul G. Fournier |
| Publisher | : |
| Total Pages | : 34 |
| Release | : 1953 |
| Genre | : Airplanes |
| ISBN | : |
Download Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 4 Book in PDF, ePub and Kindle
The results presented in the present paper are part of a program conducted to investigate the effect of wing plan form on the aerodynamic characteristics in pitch, in sideslip, and during steady roll. This paper presents the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4, a leading-edge sweep of angle of 45 degrees, and with an NACA 65A006 airfoil section parallel to the plane of symmetry.
| Author | : James W. Wiggins |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1954 |
| Genre | : Airplanes |
| ISBN | : |
Download Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives Book in PDF, ePub and Kindle
| Author | : Edward Charles Polhamus |
| Publisher | : |
| Total Pages | : 86 |
| Release | : 1960 |
| Genre | : Aerodynamics, Transonic |
| ISBN | : |
Download The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds Book in PDF, ePub and Kindle
| Author | : Edward C. Polhamus |
| Publisher | : |
| Total Pages | : 90 |
| Release | : 1955 |
| Genre | : Aerodynamics |
| ISBN | : |
Download The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds Book in PDF, ePub and Kindle
A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.
| Author | : |
| Publisher | : |
| Total Pages | : 818 |
| Release | : 1954 |
| Genre | : Aeronautics |
| ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, ePub and Kindle
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 388 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
Download Index of NACA Technical Publications Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 424 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 508 |
| Release | : 1954 |
| Genre | : Aeronautics |
| ISBN | : |
Download Research Abstracts and Reclassification Notice Book in PDF, ePub and Kindle
| Author | : Defense Documentation Center (U.S.) |
| Publisher | : |
| Total Pages | : 922 |
| Release | : 1960 |
| Genre | : Industrial arts |
| ISBN | : |
Download Subject Index to Unclassified ASTIA Documents Book in PDF, ePub and Kindle
| Author | : Douglas Aircraft Company |
| Publisher | : |
| Total Pages | : 620 |
| Release | : 1975 |
| Genre | : Airplanes |
| ISBN | : |
Download USAF Stability and Control Datcom Book in PDF, ePub and Kindle
