Download or read book Theoretical and Experimental Flow Fields for a Supersonic Cruise Fighter Forebody written by Steven F. Yaros and published by . This book was released on 1985 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Flow Field Over the Wing of a Delta wing Fighter Model with Vortex Control Devices at Mach 0 6 to 1 2 written by E. Ann Bare and published by . This book was released on 1992 with total page 146 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 1992 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Analysis of the Supersonic Flow Field about a Forebody Decelerator Combination Volume 1 Theoretical Methods and Result Comparisons written by and published by . This book was released on 1972 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: The supersonic flow field about a forebody-decelerator combination is analyzed. Tangent-cone and Newtonian methods are used to predict forebody surface pressures. Empirical correlations based on local similarity solutions predict the boundary layer characteristics, and boundary layer similarity techniques are used to predict the forebody wake parameters. The flow about a conical secondary body in the forebody wake is calculated using the method of characteristics. In Volume I the methods are presented and explained, and the results of the calculations are compared with experimental measurements; in Volume II the details of the calculation procedure and computer program are presented.
Download or read book Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1985 written by and published by . This book was released on 1986 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of a Supersonic Cruise Fighter Model Flow Field written by and published by . This book was released on 1985 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Analysis of the Supersonic Flow Field about a Forebody Decelerator Combination written by R. A. Noreen and published by . This book was released on 1972 with total page 65 pages. Available in PDF, EPUB and Kindle. Book excerpt: The supersonic flow field about a forebody-decelerator combination is analyzed. Tangent-cone and Newtonian methods are used to predict forebody surface pressures. Empirical correlations based on local similarity solutions predict the boundary layer characteristics, and boundary layer similarity techniques are used to predict the forebody wake parameters. The flow about a conical secondary body in the forebody wake is calculated using the method of characteristics. In Volume I the methods are presented and explained, and the results of the calculations are compared with experimental measurements; in Volume II the details of the calculation procedure and computer program are presented.
Download or read book Investigation of a Supersonic Cruise Fighter Model Flow Field written by David E. Reubush and published by . This book was released on 1985 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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