Download or read book Low speed Wind tunnel Tests of Fowler Flaps Slats and Nose Flaps on a Model of a Jet Aircraft with a 40 Degree Swept back Wing written by and published by . This book was released on 1948 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Wind tunnel Test of Fowler Flaps Slats and Nose Flaps on a Model of a Jet Aircraft with a 40 Deg Swept back Wing written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1952 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low Speed Wind Tunnel Tests of Fowler Flaps Slats and Nose Flaps on a Model of a Jet Aircraft with a 40 Deg Swept back Wing written by Alec SPENCE and published by . This book was released on 1948 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: "This report presents the results of tests with Fowler flaps on a model of a single-jet aircraft with a 40 deg swept-back 10 per cent thick wing. Slats and nose flaps were also tested as means of delaying the tip stall."--Author's summary.
Download or read book Low speed Wind tunnel Tests of Fowler Flaps Slats and Nose Flaps on a Model of a Jet Aircraft with a 40 Deg Swept back Wing written by A. Spence and published by . This book was released on 1948 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Wind tunnel Test of Fowler Flaps Slats and Nose Flaps on a Model of a Jet Aircraft with a 40 Deg Swept back Wing written by Great Britain Aeronautical Research Council and published by . This book was released on 1952 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low Speed Wind Tunnel Tests on a One seventh Scale Model of the H 126 Jet Flap Aircraft written by and published by . This book was released on 1975 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Wind tunnel Tests on a Sweptback Wing Model Buccaneer Mark I with Blowing at the Wing Leading Edge and Blowing Over the Flaps and Drooped Ailerons written by S. F. J. Butler and published by . This book was released on 1971 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept wing Airplane with Blowing Flaps and Leading edge Slats written by Harry A. James and published by . This book was released on 1957 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Download or read book Large scale Wind tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2 8 Employing High velocity Blowing Over the Leading and Trailing edge Flaps written by David H. Hickey and published by . This book was released on 1958 with total page 65 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Full scale Wind tunnel Tests of a 35 Degree Sweptback Wing Airplane with High velocity Blowing Over the Trailing edge Flaps written by Mark W. Kelly and published by . This book was released on 1955 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept wing Airplane with Slotted Flaps Area Suction Flaps and Wing Leading edge Devices written by Ralph L. Maki and published by . This book was released on 1957 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low Speed Wind Tunnel Test of Jet Flaps and Floating Wingtip Ailerons on a Fighter Wing written by John A. Eney and published by . This book was released on 1974 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: An 18% scale semispan fighter wing was tested at low speed in various configurations to assess improvements in lift and roll control. A full span jet flap achieved a CL 14% higher than current aircraft. Floating wingtip ailerons provided undiminished roll control up through high angles of attack. Parameters measured were angle of attack, lift coefficient, drag coefficient, pitching moment, rolling moment, and yawing moment.
Download or read book Large scale Wind tunnel Tests of an Airplane Model with Two Propellers and Rotaing Cylinder Flaps written by James A. Weiberg and published by . This book was released on 1968 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Large scale Wind tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2 8 with Area Suction Applied to Trailing edge Flaps and with Several Wing Leading edge Modifications written by David G. Koenig and published by . This book was released on 1956 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of an airplane model was conducted to determine the effect of area-suction trailing-edge flaps and several leading-edge modifications on the aerodynamic characteristics of a 45 degree sweptback wing. The wing had an aspect ratio of 2.8 and a taper ratio of 0.17. The wing was tested with a small-span constant-chord flap and, to a lesser extent, with a larger span constant-percent wing-chord flap. Area suction was applied to both flaps. Leading-edge flaps are modified leading-edge contours were tested in an effort to produce adequate leading-edge stall control. A chord extension and a fence were also tested. Part of the testing was done with a horizontal tail installed above the extended wing-chord plane. The tests were made at a Reynolds number of 10,000,000.
Download or read book Large scale Wind tunnel Tests of an Airplane Model with Four Propellers and Rotating Cylinder Flaps written by James A. Weiberg and published by . This book was released on 1970 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Full scale Wind tunnel Tests of a 35 Degree Sweptback wing Airplane with Blowing from the Shroud Ahead of the Trailing edge Flaps written by William H. Tolhurst and published by . This book was released on 1958 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation was made at full scale to determine the effect of flap location on the jet-flow momentum coefficient required to control the flap boundary layer when blowing from the wing shroud. The tests were made on a 35 degree sweptback-wing airplane at a Reynolds number of 7,500,000,based on the mean aerodynamic chord, with flap deflections of 45, 60, and 75 degrees and with pressure ratios across the blowing nozzles from 1.0 to 2.9. The data presented show the change in lift coefficient with changes in momentum coefficient for the various flap deflections, flap positions, and nozzle heights.
