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Subsonic Longitudinal And Lateral Directional Static Aerodynamic Characteristics Of A General Research Fighter Model Employing A Strake Wing Concept
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Book Synopsis Subsonic Longitudinal and Lateral-directional Static Aerodynamic Characteristics of a General Research Fighter Model Employing a Strake-wing Concept by :
Download or read book Subsonic Longitudinal and Lateral-directional Static Aerodynamic Characteristics of a General Research Fighter Model Employing a Strake-wing Concept written by and published by . This book was released on 1978 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Longitudinal and Lateral-directional Static Aerodynamic Characteristics of a General Research Fighter Configuration Employing a Jet Sheet Vortex Generator by :
Download or read book Subsonic Longitudinal and Lateral-directional Static Aerodynamic Characteristics of a General Research Fighter Configuration Employing a Jet Sheet Vortex Generator written by and published by . This book was released on 1978 with total page 198 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Longitudinal and Lateral Directional Static Aerodynamic Characteristics for a Model with Swept Back and Swept Forward Wings by : J. K. Huffman
Download or read book Subsonic Longitudinal and Lateral Directional Static Aerodynamic Characteristics for a Model with Swept Back and Swept Forward Wings written by J. K. Huffman and published by . This book was released on 1978 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Longitudinal and Lateral Aerodynamic Characteristics for a Systematic Series of Strake-wing Configurations by :
Download or read book Subsonic Longitudinal and Lateral Aerodynamic Characteristics for a Systematic Series of Strake-wing Configurations written by and published by . This book was released on 1979 with total page 246 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1976 with total page 984 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1982 with total page 1284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3 by : Howard F. Savage
Download or read book The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3 written by Howard F. Savage and published by . This book was released on 1957 with total page 662 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted to determine the effects of vertical-tail location and size on the subsonic aerodynamic characteristics of a model having a triangular wing. The wing had an aspect ratio of 3, an NACA 0003.5-63 section in the streamwise direction, and plain, trailing-edge ailerons. The wing was attached to the fuselage in either a mid or high position and an unswept horizontal tail was located on the fuselage center line. Two vertical tails were tested which had areas of 26.7 or 20.3 percent of the wing area. Each vertical tail was equipped with a rudder and had a geometric aspect ratio of 1.5, a taper ratio of 0.16, and 54 degrees of sweepback of the leading edge. Each vertical tail was tested at two different tail lengths. The wind-tunnel tests were conducted at a Reynolds number of 2.5 milMon at Mach numbers from 0.25 to 0.95.
Book Synopsis Subsonic Longitudinal and Lateral-directional Static Aerodynamic Characteristics of a Slender Wing-body Configuration by : Charles H. Fox
Download or read book Subsonic Longitudinal and Lateral-directional Static Aerodynamic Characteristics of a Slender Wing-body Configuration written by Charles H. Fox and published by . This book was released on 1988 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flow Visualization Studies of a General Research Fighter Model Employing a Strake-wing Concept at Subsonic Speeds by : James M. Luckring
Download or read book Flow Visualization Studies of a General Research Fighter Model Employing a Strake-wing Concept at Subsonic Speeds written by James M. Luckring and published by . This book was released on 1979 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1979 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Scientific and Technical Publications by :
Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1987 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Calculation of High Angle of Attack Aerodynamics of Fighter Configurations by : Chuan-Tau Edward Lan
Download or read book Calculation of High Angle of Attack Aerodynamics of Fighter Configurations written by Chuan-Tau Edward Lan and published by . This book was released on 1991 with total page 332 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computational method for unsteady aerodynamics of fighter configurations at high angles of attack is developed. The leading-edge vortices are represented by free vortex filaments which are adjusted iteratively to satisfy the force-free condition. The small-disturbance, unsteady potential equation is solved in the frequency domain for motions in pitching, plunging, flapping, side movement, rolling, and yawing oscillation in compressible flow. Computed results in rolling moment coefficients due to side acceleration are compared with data for 60-deg and 80-deg delta wings. Lateral-directional characteristics for an F-106b configuration are also compared with data obtained in forced oscillation tests. It is shown that reasonable results can be obtained by the present unsteady flow method, but not by steady flow theory. Calculation of dynamic stall effects on a rectangular wing of aspect ratio 4 is demonstrated by using experimental section data. Although no data for the wing are available, the results appear plausible. Industrial usage of this has produced mixed results. At this time, the use of these methods in a production manner is recommended.
Download or read book NASA SP. written by and published by . This book was released on 1987 with total page 324 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index by :
Download or read book Government Reports Annual Index written by and published by . This book was released on 1993 with total page 1832 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Engineering written by and published by . This book was released on 1984 with total page 446 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Book Synopsis Subsonic Longitudinal and Lateral-directional Characteristics of a Forward-swept-wing Fighter Configuration at Angles of Attack Up to 470 by : Michael J. Mann
Download or read book Subsonic Longitudinal and Lateral-directional Characteristics of a Forward-swept-wing Fighter Configuration at Angles of Attack Up to 470 written by Michael J. Mann and published by . This book was released on 1987 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1985-06 with total page 1162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
