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Book Full scale Wind tunnel Tests of a Small Unpowered Jet Aircraft with a T Tail

Download or read book Full scale Wind tunnel Tests of a Small Unpowered Jet Aircraft with a T Tail written by Paul T. Soderman and published by . This book was released on 1971 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail were investigated in a 40 x 80 ft (12.2 by 24.4 meter) wind tunnel (subsonic). Static, longitudinal, and lateral stability, and control characteristics were determined at angles of attack from -2 deg to 42 deg. The aircraft wing had 13 deg of sweep and an aspect ratio of 5.02. The aircraft was tested power off with various wing leading- and trailing-edge high lift devices. The basic configuration was tested with and without such components as engine nacelles, wing tip tanks, and empannage. Hinge-moment data were obtained and downwash angles in the horizontal-tail plane location were calculated. The data were obtained at Reynolds numbers of 4.1 million and 8.7 million based on mean aerodynamic chord. The model had static longitudinal stability through initial stall. Severe tail buffet occurred near the angle of attack for maximum lift. Above initial stall the aircraft had pronounced pitch-up, characteristic of T-tail configurations. A stable trim point was possible at angles of attack between 30 deg and 40 deg (depending on c.g. location and flap setting). Hinge-moment data showed no regions with adverse effects on stick force. Comparisons of wind-tunnel data and flight-test are presented.

Book Full scale Wind tunnel Tests of a Small Unpowered Jet Aircraft with a T tail

Download or read book Full scale Wind tunnel Tests of a Small Unpowered Jet Aircraft with a T tail written by Paul T. Soderman and published by . This book was released on 1971 with total page 93 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Large scale Wind tunnel Tests of a Circulation Plan form Aircraft with a Peripheral Jet for Lift  Thrust  and Control

Download or read book Large scale Wind tunnel Tests of a Circulation Plan form Aircraft with a Peripheral Jet for Lift Thrust and Control written by Richard K. Grief and published by . This book was released on 1963 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low Speed Wind Tunnel Testing

Download or read book Low Speed Wind Tunnel Testing written by Alan Pope and published by Wiley-Interscience. This book was released on 1984 with total page 562 pages. Available in PDF, EPUB and Kindle. Book excerpt: Good,No Highlights,No Markup,all pages are intact, Slight Shelfwear,may have the corners slightly dented, may have slight color changes/slightly damaged spine.

Book Large scale Wind tunnel Tests of an Airplane Model with an Unswept  Tilt Wing of Aspect Ration 5 5  and with Four Propellers and Blowing Flaps

Download or read book Large scale Wind tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ration 5 5 and with Four Propellers and Blowing Flaps written by James A. Weiberg and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Full scale Wind tunnel Tests of a Low aspect ratio  Straight wing Airplane with Blowing Boundary layer Control on Leading  and Trailing edge Flaps

Download or read book Full scale Wind tunnel Tests of a Low aspect ratio Straight wing Airplane with Blowing Boundary layer Control on Leading and Trailing edge Flaps written by Mark W. Kelly and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Large scale Wind tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust

Download or read book Large scale Wind tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust written by Wallace H. Deckert and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted to determine the wing stall, performance, and longitudinal stability and control characteristics of a large model of a V/STOL tilt-wing transport aircraft. The scope of the tests was limited primarily to the low-speed transitional regime.

Book Full scale Wind tunnel and Flight Tests of a Fairchild 22 Airplane Equipped with a Fowler Flap

Download or read book Full scale Wind tunnel and Flight Tests of a Fairchild 22 Airplane Equipped with a Fowler Flap written by C. H. Dearborn and published by . This book was released on 1936 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt: Full-scale wind-tunnel and flight tests were made of a Fairchild 22 airplane equipped with a Fowler flap to determine the effect of the flap on the performance and control characteristics of the airplane. In the wind-tunnel tests of the airplane with the horizontal tail surfaces removed, the flap was found to increase the maximum lift coefficietnfrom 1.27 to 2.41. In the flight tests, the flap was found to decrease the minimum speed from 58.8 to 44.4 miles per hour. The required take-off run to attain an altitude of 50 feet was reduced from 935 feet to 700 feet by the use of the flap, the minimum distance being obtained with five-sixths full deflection. The landing run from a height of 50 feet was reduced one-third. The longitudinal and directional control was adversely afected by the flap, indicating that the design of the tail surfaces is more critical with a flapped than a plain wing.

Book Large scale Wind tunnel Tests in Ground Effect of a 35   sweptback Wing Jet Transport Model Equipped with Blowing Boundary layer control Trailing and Leading edge Flaps

Download or read book Large scale Wind tunnel Tests in Ground Effect of a 35 sweptback Wing Jet Transport Model Equipped with Blowing Boundary layer control Trailing and Leading edge Flaps written by Kiyoshi Aoyagi and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Full scale Wind Tunnel Tests of a Low wing  Single engine  Light Plane with Positive and Negative Propeller Thrust and Up and Down Flap Deflection

Download or read book Full scale Wind Tunnel Tests of a Low wing Single engine Light Plane with Positive and Negative Propeller Thrust and Up and Down Flap Deflection written by Edward Seckel and published by . This book was released on 1971 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Large scale Wind tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ratio 5 5  and with Various Stall Control Devices

Download or read book Large scale Wind tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ratio 5 5 and with Various Stall Control Devices written by James A. Weiberg and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: