Download or read book The Use of Area Suction for the Purpose of Improving Trailing edge Flap Effectiveness on a 35 Degree Sweptback Wing written by Woodrow L. Cook and published by . This book was released on 1953 with total page 77 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight Tests of a Leading edge Area Suction on a Fighter type Airplane with a 35 Degree Sweptback Wing written by Richard S. Bray and published by . This book was released on 1955 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests have been made to determine the flight characteristics of an F-86F airplane equipped with a leading-edge area-suction boundary-layer-control system, and to investigate the possible operational limitations imposed on a fighter-type airplane by such an installation. The results of the flight tests are compared with those of full-scale wind-tunnel tests of a similar installation on a model incorporating F-86 wing panels. The basic porous-area distribution tested extended the full length of the wing leading edge. Suction power was provided by a modified turbosupercharger which was driven by air bled from the compressor of the airplane's jet engine.
Download or read book Investigation of the Use of Area Suction to Increase the Effectiveness of Trailing edge Flaps of Various Spans on a Wing of 45 Degree Sweepback and Aspect Ratio 6 written by Roy N. Griffin and published by . This book was released on 1956 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made of a model with a wing of 45 degree sweepback and aspect ratio of 6 to determine the aerodynamic characteristics and suction requirements for boundary-layer control by means of area suction applied to trailing-edge flaps. Included in this study were limited tests to use the differentially deflected flaps for lateral control. Flap spans extending from 0.12 b/2 to 0.50, 0.66, and 0.83 b/2 were tested at various flap deflections at 46 degrees and 65 degrees on the 0.12 to 0.50 b/2 spans with boundary-layer control applied. A limited number of the tests were made with area suction applied to the wing leading edge.
Download or read book The Use of a Leading edge Area suction Flap to Delay Separation of Air Flow from the Leading Edge of a 35 Degree Sweptback Wing written by Curt A. Holzhauser and published by . This book was released on 1953 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Use of Leading edge Area suction Flap to Delay Separation of Air Flow from the Leading Edge of a 35 Degrees Sweptback Wing written by Curt A. Holzhauser and published by . This book was released on 1954 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Application of Area Suction to Leading edge and Trailing edge Flaps on a 44 Degree Swept wing Model written by Curt A. Holzhauser and published by . This book was released on 1956 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation was conducted with a 44 degree swept-wing model to determine the effects leading- and trailing-edge area-suction flaps have on the static longitudinal characteristics of this model, and to measure the suction requirements of the flaps.
Download or read book A Flight Investigation of Area suction and Blowing Boundary layer Control on the Trailing edge Flaps of a 35 Degree Swept wing Carrier type Airplane written by Hervey C. Quigley and published by . This book was released on 1957 with total page 69 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Use of Leading edge Area Suction to Increase the Maximum Lift Coefficient of a 35 Degree Swept back Wing written by Curt A. Holzhauser and published by . This book was released on 1952 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Use of Area Suction for the Purpose of Delaying Separation of Air Flow at the Leading Edge of a 63 Degree Swept back Wing Effects of Controlling the Chordwise Distribution of Suction air Velocities written by Woodrow L. Cook and published by . This book was released on 1952 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Use of Leading edge Area Suction to Increase the Maximum Lift Coefficient of a 35 Degrees Swept back Wing written by Curt A. Holzhauser and published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Use of Area Suction for Improving the Longitudinal Characteristics of a Thin Unswept Wing fuselage Model with Leading and Trailing edge Flaps written by David G. Koenig and published by . This book was released on 1956 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to determine the effect of porous area suction applied to the knees of full-span leading-edge and part-span trailing-edge flaps installed on an unswept-wing airplane model. The wind was of aspect ratio 3 and had a modified double-wedge section with a thickness of 4.2-percent chord. For a brief test, an unswept horizontal tail was installed on the model 0.62 semispan above the exended wing-chord plane. Most of the tests were made at a Reynolds number of 9,400,000 and a Mach number of 0.11.
Download or read book Wind tunnel and flight investigations of the use of leading edge area suction for the purpose of increasing the maximum lift coefficient of a 35 degree swept wing airplane written by Curt A. Holzhauser and published by . This book was released on 1956 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects on Control Effectiveness of Systematically Varying the Size and Location of Trailing edge Flaps on a 45 Degree Sweptback Wing at a Mach Number of 1 9 written by Carl R. Jacobson and published by . This book was released on 1951 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Subject Index to Unclassified ASTIA Documents written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Use of Area Suction for the Purpose of Delaying Separation of Air Flow at the Leading Edge of a 63 Degree Swept back Wing written by Woodrow L. Cook and published by . This book was released on 1950 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Use of Area Suction for the Purpose of Delaying Separation of Air Flow at the Leading Edge of a 63 Degrees Swept back Wing written by Woodrow L. Cook and published by . This book was released on 1951 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight Tests of a Leading edge Area Suction on a Fighter type Airplane with a 35 Degrees Sweptback Wing written by Richard S. Bray and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
