Analysis Of The Flat Spin Characteristics Of A Twin Jet Swept Wing Fighter Airplane PDF Download
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Author | : Joseph R. Chambers |
Publisher | : |
Total Pages | : 44 |
Release | : 1969 |
Genre | : Airplanes |
ISBN | : |
Download Analysis of the Flat-spin Characteristics of a Twin-jet Swept-wing Fighter Airplane Book in PDF, ePub and Kindle
Factors affecting flat spin characteristics of fighter aircraft with horizontal tail surfaces.
Author | : Joseph R. Chambers |
Publisher | : |
Total Pages | : 33 |
Release | : 1969 |
Genre | : |
ISBN | : |
Download Analysis of the Flat-spin Characteristics of a Twin-jet Swept-wing Fighter Airplane Book in PDF, ePub and Kindle
Author | : Joseph R. Chambers |
Publisher | : |
Total Pages | : 60 |
Release | : 1969 |
Genre | : Aircraft |
ISBN | : |
Download Analysis of Lateral-directional Stability Characteristics of a Twin-jet Fighter Airplane at High Angles of Attack Book in PDF, ePub and Kindle
Jet fighter aircraft lateral directional stability at high angles of attack.
Author | : Sue B. Grafton |
Publisher | : |
Total Pages | : 44 |
Release | : 1971 |
Genre | : Airplanes |
ISBN | : |
Download Dynamic Stability Derivatives of a Twin-jet Fighter Model for Angles of Attack from -10 ̊to 110 ̊ Book in PDF, ePub and Kindle
A low-speed investigation was conducted to determine the dynamic stability derivatives in pitch, roll, and yaw over an angle-of-attack range of -10 [degree] to 110 [degree] for a twin-jet swept-wing fighter model. Several frequencies and amplitudes were investigated to determine the effects of these variables on the stability derivatives. The effect of the vertical and horizontal tail, and horizontal-tail incidence on the derivatives was also evaluated. The results indicate that the model exhibited stable values of damping in pitch over the entire angle-of-attack range, but marked reductions of damping in roll were measured at the stall, and unstable values of damping in yaw were present for the very high angles of attack associated with flat spins. Either removal of the horizontal or vertical tail or full up deflection of the horizontal tail eliminated the unstable characteristics of the damping-in-yaw derivatives.
Author | : |
Publisher | : |
Total Pages | : 24 |
Release | : 1960 |
Genre | : |
ISBN | : |
Download Free-Spinning-Tunnel Investigation of a 1/30 Scale Model of a Twin-Jet-Swept-Wing Fighter Airplane Book in PDF, ePub and Kindle
Author | : Edward J. Ray |
Publisher | : |
Total Pages | : 300 |
Release | : 1973 |
Genre | : Airplanes |
ISBN | : |
Download Subsonic Characteristics of a Twin-jet Swept-wing Fighter Model with Maneuvering Devices Book in PDF, ePub and Kindle
An investigation has been conducted at Mach numbers ranging from 0.06 to 0.94 to determine the effects of various combinations of leading-edge slat devices on the static aerodynamic characteristics of a twin-jet swept-wing fighter model. The study also included a determination of the effects of wing leading-edge droop, trailing-edge chord-extensions, wing fences, and wing-planform and camber modifications. The angle-of-attack range generally extended from about minus 2 deg to 24 deg and the sideslip angles ranged from about minus 6 deg to 13 deg.
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Total Pages | : |
Release | : 1969 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 604 |
Release | : 1974 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1280 |
Release | : 1980 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 796 |
Release | : 1970 |
Genre | : Mechanics, Applied |
ISBN | : |
Download Applied Mechanics Reviews Book in PDF, ePub and Kindle