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Static Aerodynamic Stability Characteristics Of A Body Of Revolution With Wraparound Fins At Mach Numbers From 05 To 13
Download Static Aerodynamic Stability Characteristics Of A Body Of Revolution With Wraparound Fins At Mach Numbers From 05 To 13 full books in PDF, epub, and Kindle. Read online Static Aerodynamic Stability Characteristics Of A Body Of Revolution With Wraparound Fins At Mach Numbers From 05 To 13 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Static Aerodynamic Stability Characteristics of a Body of Revolution with Wraparound Fins at Mach Numbers from 1.6 to 2.86 by : John E. Vaughn
Download or read book Static Aerodynamic Stability Characteristics of a Body of Revolution with Wraparound Fins at Mach Numbers from 1.6 to 2.86 written by John E. Vaughn and published by . This book was released on 1972 with total page 322 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted in the NASA Langley Unitary Plan wind tunnel for several wraparound fins with straight and with swept leading edge mounted on bodies of revolution. Mach number ranged from 1.6 to 2.86 while angle of attack was varied from -6 degrees to 6 degrees at 0 degrees sideslip angle. Six component aerodynamic force and moment data were recorded on the complete missile configuration while simultaneously recording the aerodynamic normal force and bending moments acting on each fin. The results of these tests are presented herein in plotted form. The number designation given the test is UPWT 980.
Book Synopsis Static Aerodynamic Stability Characteristics of a Body of Revolution with Wraparound Fins at Mach Numbers from 0.5 to 1.3 by : John E. Vaughn
Download or read book Static Aerodynamic Stability Characteristics of a Body of Revolution with Wraparound Fins at Mach Numbers from 0.5 to 1.3 written by John E. Vaughn and published by . This book was released on 1972 with total page 306 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted in the AEDC-4T wind tunnel for several wraparound fins with straight and with swept leading edge mounted on bodies of revolution. Mach number ranged from 0.50 to 1.30 while angle of attack was varied from -6 degrees to 6 degrees at 0 degrees sideslip angle. Six component aerodynamic force and moment data were recorded on the complete missile configuration while simultaneously recording the aerodynamic normal force and bending moments acting on each fin. The results of these tests are presented in plotted form. (Author).
Book Synopsis A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0 by : James A. Humphrey
Download or read book A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0 written by James A. Humphrey and published by . This book was released on 1977 with total page 234 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wrap-around fin effectiveness for tube-launched missiles was investigated in a series of 6 wind tunnel tests. Wind tunnels were AEDC Propulsion Wind Tunnel, NASA/Langley Research Center Unitary Plan Wind Tunnel and McDonnell Douglas 4-foot Trisonic Wind Tunnel. Mach number range was 0.3 to 3.0. Basic model was a 2-caliber secant ogive nose with an 8-caliber cylindrical afterbody and 21 fin configurations. Variations in the coefficients are presented for changes in fin geometry including taper ratio and leading edge sweep angle, aspect ratio, exposed semi-span, and root chord length; opening angle, fully closed to 10 deg past fully open; and body step down.
Book Synopsis Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Their Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3. Volume I. by :
Download or read book Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Their Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3. Volume I. written by and published by . This book was released on 1972 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: AMCDR-1001-Vol-1See also Volume 2, AD-772 670.*Guided missiles, *Fins, Tube launched, Aerodynamic forces, Pitch(Motion), Roll, Yaw, Angle of attackWraparound finsExperimental aerodynamic investigations were conducted for several wraparound fins and one planar fin configuration on bodies of revolution at Mach number ranging from 0.3 to 1.3 and angles of attack from -6 degrees to 6 degrees at 0 degrees at sideslip angle. Six component aerodynamic forces and moments were recorded on the complete missile configuration while simultaneously measuring the aerodynamic normal force and bending moments acting on each fin. The fin configuration parameters varied include chord length, fin thickness, leading edge configuration, tip chord geometry and body, root chord gap. The report presents the plotted coefficient data in two volumes. Volume I contains the complete missile aerodynamic data. (Modified author abstract).
Book Synopsis Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Their Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3. Volume II. by :
Download or read book Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Their Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3. Volume II. written by and published by . This book was released on 1972 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: OL-2AMCDR-1001-Vol-2See also Volume 1, AD-772 669.*Guided missiles, *Fins, Tube launched, Aerodynamic forces, Pitch(Motion), Roll, Yaw, Angle of attackWraparound finsExperimental aerodynamic investigations were conducted for several wraparound fins and one planar fin configuration on bodies of revolution at Mach number ranging from 0.3 to 1.3 and angles of attack from -6 degrees to 6 degrees at 0 degrees sideslip angle. Six component aerodynamic forces and moments were recorded on the complete missile configuration while simultaneously measuring the aerodynamic normal force and bending moments acting on each fin. The fin configuration parameters varied include chord length, fin thickness, leading edge configuration, tip chord geometry and body, root chord gap. The report presents the plotted coefficient data in two volumes. Volume 2 contains the individual fin aerodynamic data. (Modified author abstract).
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 with total page 994 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Effects of Fin Plan Form on the Static Stability of Fin-body Combinations at Mach Number 4.06 by : Edward F. Ulmann
Download or read book Some Effects of Fin Plan Form on the Static Stability of Fin-body Combinations at Mach Number 4.06 written by Edward F. Ulmann and published by . This book was released on 1952 with total page 28 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 1977 with total page 1276 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Government Reports Index written by and published by . This book was released on 1975 with total page 1262 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 by : Ross B. Robinson
Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Cross-section Distribution on the Static Stability Characteristics of Axi-symmetric Bodies at Mach Numbers of 5.35 and 6.71 by : J. F. Reilly
Download or read book The Effect of Cross-section Distribution on the Static Stability Characteristics of Axi-symmetric Bodies at Mach Numbers of 5.35 and 6.71 written by J. F. Reilly and published by . This book was released on 1966 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made at hypersonic Mach numbers to determine the effects of cross-section distribution on the static stability characteristics of bodies of revolution and to obtain the aerodynamic characteristics of these bodies. All of the bodies tested had the same length and all were circular in cross-section. The bodies tested were conic, bi-conic, and tri-conic. The tests were performed at Mach numbers of 5.35 and 6.71, and at unit Reynolds numbers from 1.5 x 100,000 to 3.2 x 100,000 per centimeter. The results indicate that under certain test conditions a body with a forecone followed by a frustum or frustum-flare combination exhibits, through the flow mechanism on the upper quarter of the body, an adverse center of pressure travel in the low angle of attack region (0 to 5 degrees). For a given moment reference point this yields both stable and unstable trim-points. (Author).
Download or read book AIAA 82-0302 - AIAA 82-0351 written by and published by . This book was released on 1982 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5 by :
Download or read book Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5 written by and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Collection of Technical Papers on Atmospheric Flight Mechanics by :
Download or read book Collection of Technical Papers on Atmospheric Flight Mechanics written by and published by . This book was released on 1974 with total page 330 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Systematic Study of the Static Stability Characteristics of a Series of Afterbody Flare, Fin, and Boattail Configurations at Mach Numbers from 1.57 to 2.87 by :
Download or read book Systematic Study of the Static Stability Characteristics of a Series of Afterbody Flare, Fin, and Boattail Configurations at Mach Numbers from 1.57 to 2.87 written by and published by . This book was released on 1959 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of the National Science Council, Republic of China by :
Download or read book Proceedings of the National Science Council, Republic of China written by and published by . This book was released on 1979 with total page 514 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings by : Guo jia ke xue wei yuan hui
Download or read book Proceedings written by Guo jia ke xue wei yuan hui and published by . This book was released on 1979 with total page 514 pages. Available in PDF, EPUB and Kindle. Book excerpt:
