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Experimental And Theoretical Study Of Aerodynamic Characteristics Of Some Lifting Bodies At Angles Of Attack From 10 Degrees To 53 Degrees At Mach Numbers From 230 To 462
Download Experimental And Theoretical Study Of Aerodynamic Characteristics Of Some Lifting Bodies At Angles Of Attack From 10 Degrees To 53 Degrees At Mach Numbers From 230 To 462 full books in PDF, epub, and Kindle. Read online Experimental And Theoretical Study Of Aerodynamic Characteristics Of Some Lifting Bodies At Angles Of Attack From 10 Degrees To 53 Degrees At Mach Numbers From 230 To 462 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Degrees to 53 Degrees at Mach Numbers from 2.30 to 4.62 by : M. Leroy Spearman
Download or read book Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Degrees to 53 Degrees at Mach Numbers from 2.30 to 4.62 written by M. Leroy Spearman and published by . This book was released on 1994 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722218300 Total Pages :28 pages Book Rating :4.2/5 (183 download)
Book Synopsis Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Degrees to 53 Degrees at Mach Numbers from 2. 30 To 4. 62 by : National Aeronautics and Space Administration (NASA)
Download or read book Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Degrees to 53 Degrees at Mach Numbers from 2. 30 To 4. 62 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-03 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lifting bodies are of interest for possible use as space transportation vehicles because they have the volume required for significant payloads and the aerodynamic capability to negotiate the transition from high angles of attack to lower angles of attack (for cruise flight) and thus safely reenter the atmosphere and perform conventional horizontal landings. Results are presented for an experimental and theoretical study of the aerodynamic characteristics at supersonic speeds for a series of lifting bodies with 75 deg delta planforms, rounded noses, and various upper and lower surface cambers. The camber shapes varied in thickness and in maximum thickness location, and hence in body volume. The experimental results were obtained in the Langley Unitary Plan Wind Tunnel for both the longitudinal and the lateral aerodynamic characteristics. Selected experimental results are compared with calculated results obtained through the use of the Hypersonic Arbitrary-Body Aerodynamic Computer Program. Spearman, M. Leroy and Torres, Abel O. Langley Research Center RTOP 505-69-20-01...
Book Synopsis Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Deg to 53 Deg at Mach Numbers from 2.30 to 4.62 by : M. Leroy Spearman
Download or read book Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Deg to 53 Deg at Mach Numbers from 2.30 to 4.62 written by M. Leroy Spearman and published by . This book was released on 1994 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 to 53 at Mach Numbers from 2.30 to 4.62 by : M. Leroy Spearman
Download or read book Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 to 53 at Mach Numbers from 2.30 to 4.62 written by M. Leroy Spearman and published by . This book was released on 1994 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -100 to 530 at Mach Numbers from 2.30 to 4.62 by :
Download or read book Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -100 to 530 at Mach Numbers from 2.30 to 4.62 written by and published by . This book was released on 1994 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation at a Mach Number of 3.11 of the Lift, Drag, and Pitching-moment Characteristics of Five Blunt Lifting Bodies by : William Letko
Download or read book Experimental Investigation at a Mach Number of 3.11 of the Lift, Drag, and Pitching-moment Characteristics of Five Blunt Lifting Bodies written by William Letko and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Aerodynamic Characteristics of Some Lifting Bodies by : David H. Dennis
Download or read book The Aerodynamic Characteristics of Some Lifting Bodies written by David H. Dennis and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Blunted Right Triangular Pyramidal Lifting Reentry Configuration for Angles of Attack Up to 110° by : John P. Mugler
Download or read book Static Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Blunted Right Triangular Pyramidal Lifting Reentry Configuration for Angles of Attack Up to 110° written by John P. Mugler and published by . This book was released on 1961 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings and Tail at Angles of Attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0 by : Leland H. Jorgensen
Download or read book Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings and Tail at Angles of Attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1976 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for Bodies of Elliptic Cross Section at Angles of Attack from 0 O to 58 O and Mach Numbers from 0.6 to 2.0 by : Leland H. Jorgensen
Download or read book Experimental Aerodynamic Characteristics for Bodies of Elliptic Cross Section at Angles of Attack from 0 O to 58 O and Mach Numbers from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1975 with total page 77 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in the Ames 6- by 6-Foot Wind Tunnel to measure the static aerodynamic characteristics for two bodies of elliptic cross section and for their equivalent body of revolution. The equivalent body of revolution had the same length and axial distribution of cross-sectional area as the elliptic bodies. It consisted of a tangent ogive nose of fineness ratio 3 followed by a cylinder with a fineness ratio of 7. For the first body of elliptic cross section, the ratio of the semimajor axis to semiminor axis was held constant at 2 all along the body length. For the second elliptic body the nose was unchanged, but the aftersection was changed as follows: The cross-sectional axis ratio a/b was decreased from 2 to 1 over an axial distance of about 1.66 diam. Then, at this position, the a, b axis system was rotated 90°, and the a/b ratio was increased back to 2 over the next 2.34 diam in length. Over the last length of three body diam, this rotated a/b ratio was held constant at 2.
Book Synopsis Experimental Aerodynamic Characteristics for Bodies of Elliptic Cross Section at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0 by : Leland H. Jorgensen
Download or read book Experimental Aerodynamic Characteristics for Bodies of Elliptic Cross Section at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1975 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics in Pitch of Several Ring-wing-body Configurations at a Mach Number of 2.2 by : Odell A. Morris
Download or read book Aerodynamic Characteristics in Pitch of Several Ring-wing-body Configurations at a Mach Number of 2.2 written by Odell A. Morris and published by . This book was released on 1962 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Some Lifting Reentry Concepts Applicable to Transatmospheric Vehicle Design Studies by :
Download or read book Aerodynamic Characteristics of Some Lifting Reentry Concepts Applicable to Transatmospheric Vehicle Design Studies written by and published by . This book was released on 1984 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0 by : Leland H. Jorgensen
Download or read book Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1976 with total page 121 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings and Tail at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0 by : Leland Howard Jorgensen
Download or read book Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings and Tail at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0 written by Leland Howard Jorgensen and published by . This book was released on 1976 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Control-surface Instabilities on Lifting-body Reentry Vehicles at a Mach Number of 15.4 by : Robert Charles Goetz
Download or read book Investigation of Control-surface Instabilities on Lifting-body Reentry Vehicles at a Mach Number of 15.4 written by Robert Charles Goetz and published by . This book was released on 1971 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High Angle of Attack Aerodynamics by : Josef Rom
Download or read book High Angle of Attack Aerodynamics written by Josef Rom and published by . This book was released on 1991 with total page 424 pages. Available in PDF, EPUB and Kindle. Book excerpt:
