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Author : W. Kreuger
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Wind Tunnel Investigations on a 35 Degrees Swept-back Wing with Different High-lift Devices written by W. Kreuger and published by . This book was released on 1946 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : W. Kreuger
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Wind-tunnel Investigations on a 35 Degrees Swept-back Wing with Various High-lift Devices written by W. Kreuger and published by . This book was released on 1947 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : W. Kreuger
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Wind Tunnel Investigations on a 35 Degree Swept-back Wing with Different High-lift Devices written by W. Kreuger and published by . This book was released on 1946 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael F. Marx
Publisher :
ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.:/5 (437 download)
Download or read book Low Speed Wind Tunnel Investigation of High Lift Devices on a 65 Degree Swept-back Supersonic Wing of 3.44 Aspect Ratio written by Michael F. Marx and published by . This book was released on 1949 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Curt A. Holzhauser
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (17 download)
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:
Author : William Koven
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.:/5 (11 download)
Download or read book Wind-tunnel Investigation of High-lift and Stall-control Devices on a 37 Degrees Sweptback Wing of Aspect Ratio 6 at High Reynolds Numbers written by William Koven and published by . This book was released on 1948 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John G. Lowry
Publisher :
ISBN 13 :
Total Pages : 9 pages
Book Rating : 4.:/5 (11 download)
Download or read book Low-speed Wind-tunnel Investigation of a Jet Control on a 35 Degree Swept Wing written by John G. Lowry and published by . This book was released on 1953 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James A. Weiberg
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (11 download)
Download or read book Wind-tunnel Investigation at L; Ow Speed of a Wing Swept Back 63 Degrees and Twisted and Cambered for Uniform Load at a Lift Coefficient of 0.5 and with a Thickened Tip Section written by James A. Weiberg and published by . This book was released on 1950 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : David H. Hickey
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.:/5 (31 download)
Download or read book Large-scale Wind-tunnel Tests and Evaluation of the Low-speed Performance of a 35 Degree Sweptback Wing Jet Transport Model Equipped with a Blowing Boundary-layer-control Flap and Leading Edge Slat written by David H. Hickey and published by . This book was released on 1960 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : D.A. Lovell
Publisher :
ISBN 13 :
Total Pages : 194 pages
Book Rating : 4.:/5 (11 download)
Download or read book A Wind-tunnel Investigation of the Effects of Flap Span and Deflection Angle, Wing Planform and the High-lift Performance of a 28 Degrees Swept Wing written by D.A. Lovell and published by . This book was released on 1976 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John A. Kelly
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)
Download or read book Aerodynamic Characteristics of a Leading-edge Slat on a 35 Degree Swept-back Wing for Mach Numbers from 0.30 to 0.88 written by John A. Kelly and published by . This book was released on 1951 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The data presented in this report were obtained by North American Aviation, Inc., from an investigation conducted in the Southern California Cooperative Wind Tunnel. Tests were made over a range of Mach numbers from 0.300 to 0.883 to determine the aerodynamic characteristics of a semispan model of a 35 degree swept-back wing equipped with a leading-edge slat and to gain additional knowledge of the aerodynamic loads and automatic operation of the slat. Lift, drag, and pitching-moment characteristics of a model wing in the presence of a fuselage were measured as well as pressures acting on the slat in the retracted and the full-open positions. The pressure data were analyzed to ascertain the opening characteristics of the slat for two possible circular-arc slat tracks which could be used for automatic operation of the slat.
Author : M.J. Queijo
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (11 download)
Download or read book Wind-tunnel Investigation at Low Speed of the Effects of Chordwise Wing Fences and Horizontal-tail Position on the Static Longitudinal Stability Characteristics of an Airplane Model with a 35 Degree Sweptback Wing written by M.J. Queijo and published by . This book was released on 1954 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James A. Weiberg
Publisher :
ISBN 13 :
Total Pages : 53 pages
Book Rating : 4.:/5 (11 download)
Download or read book Wind-tunnel Investigation at Low Speed of a Wing Swept Back 63 Degrees and Twisted and Cambered for a Uniform Load at a Lift Coefficient of 0.5 written by James A. Weiberg and published by . This book was released on 1950 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James A. Weilberg
Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (317 download)
Download or read book Wind Tunnel Investigation at Low Speed of a Twisted and Cambered Wing Swept Back 63 Degrees with Vortex Generators and Fences written by James A. Weilberg and published by . This book was released on 1952 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Hans Olaf Palme
Publisher :
ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (145 download)
Download or read book Summary of wind tunnel data for high-lift devices on swept wings written by Hans Olaf Palme and published by . This book was released on 1953 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Stanley F. Racisz
Publisher :
ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (11 download)
Download or read book Wind-tunnel Investigation at High and Low Subsonic Mach Numbers of a Thin Sweptback Wing Having an Airfoil Section Designed for High Maximum Lift written by Stanley F. Racisz and published by . This book was released on 1952 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Richard S. Bray
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.3/5 (91 download)
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.
