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Book Flight Tests of a Leading edge Area Suction on a Fighter type Airplane with a 35 Degree Sweptback Wing

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.

Book Flight Measurements of the Low speed Characteristics of a 35 Degree Swept wing Airplane with Area Suction Boundary layer Control on the Flaps

Download or read book Flight Measurements of the Low speed Characteristics of a 35 Degree Swept wing Airplane with Area Suction Boundary layer Control on the Flaps written by Seth B. Anderson and published by . This book was released on 1956 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests have been conducted to determine the flight characteristics of an F-86A airplane equipped with an area-suction boundary-layer-control system on the flaps, and to investigate the possible operational problems which may arise on a flight installation of boundary-layer control. The effectiveness of the flap was determined in conjunction with the normal slatted leading edge (open and closed) and a modified leading edge incorporating camber and an increased leading-edge radius. Measurements were made of the lift, drag, and to a limited extent, of the suction requirements. Performance computations were made to show the effect of boundary-layer control on take-off, climb, and landing. 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 and a modified flap.

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

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:

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

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:

Book Flight Investigation of the Low Speed Characteristics of a 45 Deg Swept Wing Fighter Type Airplane with Blowing Boundary Layer Control Applied to the Leading  and Trailing Edge Flaps

Download or read book Flight Investigation of the Low Speed Characteristics of a 45 Deg Swept Wing Fighter Type Airplane with Blowing Boundary Layer Control Applied to the Leading and Trailing Edge Flaps written by and published by . This book was released on 1960 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Preliminary Report on Flight Tests of an Airplane Having Exhaust heated Wings

Download or read book Preliminary Report on Flight Tests of an Airplane Having Exhaust heated Wings written by Lewis A. Rodert and published by . This book was released on 1941 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flights have been made with an airplane in icing conditions in order to test the effect of exhaust heat applied to the wings as a means of preventing ice formations. Other ice-prevention equipment, including an exhaust gas-heated pitot-static head, hot-air-heated windshield, and an inflatable de-icer of recent design, were also tested.

Book A Flight Investigation of the Practical Problems Associated with Porous leading edge Suction

Download or read book A Flight Investigation of the Practical Problems Associated with Porous leading edge Suction written by Paul A. Hunter and published by . This book was released on 1954 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flight investigation has been made of the practical problems associated with the use of porous-leading-edge suction. The wing leading edge of the test airplane was porous over approximately 83 percent of the span and the first 8 percent of the chord of the upper surface. Various other extents of suction area within these limits were also tested.

Book Flight Investigation of the Low speed Characteristics of a 45 Degree Swept wing Fighter type Airplane with Blowing Boundary layer Control Applied to the Trailing edge Flaps

Download or read book Flight Investigation of the Low speed Characteristics of a 45 Degree Swept wing Fighter type Airplane with Blowing Boundary layer Control Applied to the Trailing edge Flaps written by Hervey C. Quigley and published by . This book was released on 1958 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low Speed Flight Characteristics of a Variable Wing Sweep Fighter Model

Download or read book Low Speed Flight Characteristics of a Variable Wing Sweep Fighter Model written by and published by . This book was released on 1965 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind Tunnel Tests on a Swept Back Wing Having Distributed Suction on the Leading Edge

Download or read book Wind Tunnel Tests on a Swept Back Wing Having Distributed Suction on the Leading Edge written by E. D. Poppleton and published by . This book was released on 1950 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book IRE Transactions on Human Factors in Electronics

Download or read book IRE Transactions on Human Factors in Electronics written by Institute of Radio Engineers. Professional Group on Human Factors in Electronics and published by . This book was released on 1960 with total page 730 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effect of Area suction type Boundary layer Control on the Landing approach Characteristics of a 35 Degree Swept wing Fighter

Download or read book Effect of Area suction type Boundary layer Control on the Landing approach Characteristics of a 35 Degree Swept wing Fighter written by George E. Cooper and published by . This book was released on 1956 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Flight Investigation of the Low speed Characteristics of a 45   Swept wing Fighter type Airplane with Blowing Boundary layer Control Applied to the Leading  and Trailing edge Flaps

Download or read book Flight Investigation of the Low speed Characteristics of a 45 Swept wing Fighter type Airplane with Blowing Boundary layer Control Applied to the Leading and Trailing edge Flaps written by Hervey C. Quigley and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: