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Effect Of Missile Nose Length And Shape On Fin Effectiveness
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Book Synopsis Effect of Missile Nose Length and Shape on Fin Effectiveness by : Donald V. Rubin
Download or read book Effect of Missile Nose Length and Shape on Fin Effectiveness written by Donald V. Rubin and published by . This book was released on 1970 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel investigation of the effect of missile nose length and shape on fin aerodynamics was conducted using four nose configurations in combination with five fin configurations. The distance between the nose and the fins was varied by using two body spacers. Total model length varied from 8.5 to 13.5 calibers. The tests were conducted at Mach numbers from 1.75 to 4.5 at an angle of attack range of -4 to 16 degrees. The effects of nose length and shape on missile normal force, center of pressure, and axial force are shown. (Author).
Book Synopsis Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86 by : Lloyd S. Jernell
Download or read book Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86 written by Lloyd S. Jernell and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins by : William J. Monta
Download or read book Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins written by William J. Monta and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missle Configuration at Mach 1.550 to 2.86 by : Lloyd S. Jernell
Download or read book Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missle Configuration at Mach 1.550 to 2.86 written by Lloyd S. Jernell and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numbers from 0.80 to 4.50 by : Donald J. Spring
Download or read book The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numbers from 0.80 to 4.50 written by Donald J. Spring and published by . This book was released on 1964 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Nose Bluntness and Afterbody Shape on Aerodynamic Characteristics of a Monoplanar Missile Concept with Bodies of Circular and Elliptical Cross Sections at a Mach Number of 2.50 by : Ernald B. Graves
Download or read book Effect of Nose Bluntness and Afterbody Shape on Aerodynamic Characteristics of a Monoplanar Missile Concept with Bodies of Circular and Elliptical Cross Sections at a Mach Number of 2.50 written by Ernald B. Graves and published by . This book was released on 1979 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Numerical Investigation of Aerodynamics of Canard-controlled Missile Using Planar and Grid Tail Fins by : James DeSpirito
Download or read book Numerical Investigation of Aerodynamics of Canard-controlled Missile Using Planar and Grid Tail Fins written by James DeSpirito and published by . This book was released on 2004 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt: Viscous computational fluid dynamic simulations were used to predict the aerodynamic coefficients and flow field around a canard-controlled missile in subsonic and transonic flow. Computations were performed at Mach 0.6 and 0.9, six angles of attack between 0 deg and 10 deg, and with planar and grid tail fins. The computations were validated with wind tunnel data. Flow visualizations showed that the canard downwash produced a low-pressure region on the starboard side of the missile that produced a large induced side force. The canard trailing vortices interacted with the tail fins until alpha> 8 deg, producing a pressure differential on the leeward tail fin, leading to the adverse induced roll effects. Visualizations of the flow through the grid fin structure showed choking of the flow at Mach 0.9 and Mach 1.5. The validated simulations results showed that grid fins did not improve the canard roll-control effectiveness at subsonic and transonic speeds as well as they did at the low supersonic speed.
Book Synopsis Normal Force Effectiveness of Several Fin Planforms with Streamwise Gaps at Mach Numbers of 0.8 to 5.0 by : C. W. Dahlke
Download or read book Normal Force Effectiveness of Several Fin Planforms with Streamwise Gaps at Mach Numbers of 0.8 to 5.0 written by C. W. Dahlke and published by . This book was released on 1970 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report contains the results and analysis of a series of wind-tunnel tests for several rectangular and one delta fin planform with streamwise gaps between the fin root chord and body. The tests were conducted at free-stream Mach numbers from 0.8 to 1.5 with fin to body gap variation of 0.00 to 0.25 body diameter. The normal force effectiveness for the fin-gap configuration is presented as normal force coefficient slopes at zero angle of attack. Small gaps are shown to cause significant loss in fin effectiveness especially at transonic Mach numbers. (Author).
Author :Jack Norman Nielsen Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 :9780962062902 Total Pages :450 pages Book Rating :4.0/5 (629 download)
Book Synopsis Missile Aerodynamics by : Jack Norman Nielsen
Download or read book Missile Aerodynamics written by Jack Norman Nielsen and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1988-01-01 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt: The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. " Missile Aerodynamics," a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more. J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc.
Book Synopsis Effect of Nose Shape and Wing Thickness Ratio on the Drag at Zero Lift of a Missile Having Triangular Wings and Tails by : James R. Hall
Download or read book Effect of Nose Shape and Wing Thickness Ratio on the Drag at Zero Lift of a Missile Having Triangular Wings and Tails written by James R. Hall and published by . This book was released on 1950 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of 0.187-scale Model of a Target Missile at Mach 1.80 to 2.16 by : William A. Corlett
Download or read book Aerodynamic Characteristics of 0.187-scale Model of a Target Missile at Mach 1.80 to 2.16 written by William A. Corlett and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Nose Shape and Tail Length on Supersonic Stability Characteristics of a Projectile by : Wallace C. Sawyer
Download or read book Effect of Nose Shape and Tail Length on Supersonic Stability Characteristics of a Projectile written by Wallace C. Sawyer and published by . This book was released on 1973 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Handbook of Model Rocketry by : George Harry Stine
Download or read book The Handbook of Model Rocketry written by George Harry Stine and published by Prentice Hall. This book was released on 1983 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt: This National Association of Rocketry handbook covers designing and building your first model rocket to launching and recovery techniques, and setting up a launch area for competition.
Book Synopsis AIR FORCE MANUAL 52-31 GUIDED MISSILES FUNDAMENTALS by : U.S. Air Force
Download or read book AIR FORCE MANUAL 52-31 GUIDED MISSILES FUNDAMENTALS written by U.S. Air Force and published by Jeffrey Frank Jones. This book was released on 1956-12-31 with total page 581 pages. Available in PDF, EPUB and Kindle. Book excerpt: I scanned the original manual at 600 dpi.
Book Synopsis Guided Missiles by : United States. Department of the Air Force
Download or read book Guided Missiles written by United States. Department of the Air Force and published by . This book was released on 1957 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect on Tail-fin Span on Stability and Control Characteristics of a Canard-controlled Missile at Supersonic Mach Numbers by : A. B. Blair
Download or read book Effect on Tail-fin Span on Stability and Control Characteristics of a Canard-controlled Missile at Supersonic Mach Numbers written by A. B. Blair and published by . This book was released on 1983 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Design Aerodynamic Prediction Methodology for Missiles with Nose Bluntness by : Charles W. Ingram
Download or read book Preliminary Design Aerodynamic Prediction Methodology for Missiles with Nose Bluntness written by Charles W. Ingram and published by . This book was released on 1978 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt: A semi-empirical methodology is presented for predicting the axial and normal force coefficients and the center of pressure to include nose bluntness effects for missiles. This methodology includes the transonic and supersonic Mach number regime with angles of attack from 0 to 180 degrees. This methodology correlates well with wind tunnel test data. (Author).
