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Aerodynamic Characteristics Of Multiple Fins At Supersonic Mach Numbers
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Book Synopsis Aerodynamic Characteristics of Multiple Fins at Supersonic Mach Numbers by : Klaus O. Opalka
Download or read book Aerodynamic Characteristics of Multiple Fins at Supersonic Mach Numbers written by Klaus O. Opalka and published by . This book was released on 1969 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt: Selected test data are presented which show the aerodynamic properties of multiple fins, mounted on the tail section of slender bodies of revolution, as a function of the fin geometry at Mach numbers 1.75, 2.50, 3.50 and 4.50. Other parameters which alter the flow field past the fins such as the length of the forebody, the shape of the nose and the location of canard fins are also considered. (Author).
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing by : Edward J. Ray
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Low Aspect Ratio Fins at Mach Numbers from 0.80 to 1.30 by : D.K. Smith
Download or read book Aerodynamic Characteristics of Low Aspect Ratio Fins at Mach Numbers from 0.80 to 1.30 written by D.K. Smith and published by . This book was released on 1971 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Several Low Aspect Ratio Stabilizer Fins at Mach Numbers from 0.8 to 1.3 by : J. M. Whoric
Download or read book Aerodynamic Characteristics of Several Low Aspect Ratio Stabilizer Fins at Mach Numbers from 0.8 to 1.3 written by J. M. Whoric and published by . This book was released on 1972 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic characteristics of ogive oversize-head cylinders stabilized by tail-mounted, multiple fins or ring wings at supersonic mach numbers by : Klaus O. Opalka
Download or read book Aerodynamic characteristics of ogive oversize-head cylinders stabilized by tail-mounted, multiple fins or ring wings at supersonic mach numbers written by Klaus O. Opalka and published by . This book was released on 1973 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: Test data are reported for two ring-wing and two multiple-fin stabilizers mounted on the tail of a cylinder combined with ogive oversize heads of 1.38 caliber diameter and varying lengths. Wind tunnel tests were run at five (5) Mach numbers from 1.75 to 3.5 and the resulting aerodynamic coefficients are plotted versus angle of attack and Mach number. The results are discussed regarding their effects on the longitudinal stability for the various configurations. (Author).
Book Synopsis Investigation of the Aerodynamic Characteristics at High Supersonic Mach Numbers of a Family of Delta Wings Having Double-wedge Sections with the Maximum Thickness at 0.18 Chord by : Mitchel H. Bertram
Download or read book Investigation of the Aerodynamic Characteristics at High Supersonic Mach Numbers of a Family of Delta Wings Having Double-wedge Sections with the Maximum Thickness at 0.18 Chord written by Mitchel H. Bertram and published by . This book was released on 1954 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: A program to investigate the aerodynamic characteristics of a family of delta wings with a blunt double-wedge section has been conducted at the Langley 11-inch hypersonic tunnel. These wings had a maximum thickness of 8 percent of the chord located at the 18-percent-chord point. For the wings tested at a Mach number of 6.9, the semiapex angle was varied from 5 to 30 degrees and the wings were tested over a range of angle of attack from 0 to 28 degrees and Reynolds numbers in the range of 800,000 to 3,600,000 based on root chord. In addition, pertinent results from tests at Mach number as low as 1.62 have been utilized. The shock-expansion theory and the Newtonian impact theory have been used to analyze the effects of changes made in the various parameters investigated.
Book Synopsis Investigation of the Aerodynamic Characteristics of a Supersonic Horizontal- Attitude VTOL Airplane Model at Mach Numbers of 1.57, 2.14, 2.54, and 2.87 by : Arthur E. Franklin
Download or read book Investigation of the Aerodynamic Characteristics of a Supersonic Horizontal- Attitude VTOL Airplane Model at Mach Numbers of 1.57, 2.14, 2.54, and 2.87 written by Arthur E. Franklin and published by . This book was released on 1960 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20 by : Clyde Hayes
Download or read book Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20 written by Clyde Hayes and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.63 of a Supersonic Transport Model with a Variable-sweep M Wing by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.63 of a Supersonic Transport Model with a Variable-sweep M Wing written by and published by . This book was released on 1965 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers 2.30, 2.60, and 2.96 of a Supersonic Transport Model Having a Fixed, Warped Wing by :
Download or read book Aerodynamic Characteristics at Mach Numbers 2.30, 2.60, and 2.96 of a Supersonic Transport Model Having a Fixed, Warped Wing written by and published by . This book was released on 1965 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Subsonic and Supersonic Mach Numbers of a Thin Triangular Wing of Aspect Ratio 2 by : Harold J. Walker
Download or read book Aerodynamic Characteristics at Subsonic and Supersonic Mach Numbers of a Thin Triangular Wing of Aspect Ratio 2 written by Harold J. Walker and published by . This book was released on 1948 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: The lift, drag, and pitching-moment characteristics of a triangular wing, having an aspect ratio of 2 and a symmetrical double-wedge profile of 5-percent-chord maximum thickness at midchord, have been evaluated from wind-tunnel tests at Mach numbers from 0.50 to 0.975 and from 1.09 to 1.49 and at Reynolds numbers ranging from 0.67 to 0.85 million.
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight written by and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamic Characteristics of a Circular Body Earth-to-orbit Vehicle by : George M. Ware
Download or read book Supersonic Aerodynamic Characteristics of a Circular Body Earth-to-orbit Vehicle written by George M. Ware and published by . This book was released on 1994 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.6 to 2.16 of Supersonic Cruise Fighter Configuration with a Design Mach Mumber of 1.8 by : Barrett L. Shrout
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.6 to 2.16 of Supersonic Cruise Fighter Configuration with a Design Mach Mumber of 1.8 written by Barrett L. Shrout and published by . This book was released on 1977 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.70 of Two Supersonic Cruise Fighter Configurations by : Samuel M. Dollyhigh
Download or read book Experimental Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.70 of Two Supersonic Cruise Fighter Configurations written by Samuel M. Dollyhigh and published by . This book was released on 1979 with total page 187 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing written by and published by . This book was released on 1964 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Subsonic and Supersonic Mach Numbers of a Thin Triangular Wing of Aspect Ratio 2 by : Robert E. Berggren
Download or read book Aerodynamic Characteristics at Subsonic and Supersonic Mach Numbers of a Thin Triangular Wing of Aspect Ratio 2 written by Robert E. Berggren and published by . This book was released on 1948 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of a wind-tunnel investigation conducted to determine the effects of Mach number on the aerodynamic characteristics of a wing of triangular plan form. The wing was of aspect ratio 2 and of symmetrical double-wedge section with 5-percent chord maximum thickness at 20 percent of the chord. The tests were conducted at Mach numbers from 0.50 to 0.975 and 1.09 to 1.49 and at Reynolds numbers ranging from 0.67 to 0.85 million.
