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Some Effects Of Fin Plan Form On The Static Stability Of Fin Body Combinations At Mach Number 406
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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 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 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Several Nose and Vertical-fin Modifications on the Low-angle-of-attack Static Stability of a Winged Reentry Vehicle at Mach Numbers of 9.6 in Air and 17.8 in Helium by :
Download or read book Effects of Several Nose and Vertical-fin Modifications on the Low-angle-of-attack Static Stability of a Winged Reentry Vehicle at Mach Numbers of 9.6 in Air and 17.8 in Helium written by and published by . This book was released on 1961 with total page 52 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 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 Effect Opf 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 Opf 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 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-body Combinations of Sonic Design with Diamond, Delta and Arrow Plan Forms by : George H. Holdaway
Download or read book Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-body Combinations of Sonic Design with Diamond, Delta and Arrow Plan Forms written by George H. Holdaway and published by . This book was released on 1960 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Normal Force on Fin-Flare Combinations at Mach Numbers from 1.1 to 4.5 by : James Robert Burt (Jr)
Download or read book Normal Force on Fin-Flare Combinations at Mach Numbers from 1.1 to 4.5 written by James Robert Burt (Jr) and published by . This book was released on 1970 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of normal force on several slender fin-flare combinations is presented. The configurations were tested at Mach numbers of 1.1, 1.2, 1.3, 1.4, 1.5, 1.75, 2.5, 3.5, and 4.5. Angle of attack was carried from about -6.5 to 8.5 degrees. The effects due to varying Mach number on total model normal force and normal force due to the fins plus fin-body flow field interference are shown. Estimates of normal force of the fins plus fin-body interference are made from linearized small perturbation theory and compared to the test results. (Author).
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 Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form - Effects of Various Tail Arrangements on Wing-on and Wing-off Static Longitudinal and Lateral Stability Characteristics by : Robert W. Dunning
Download or read book Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form - Effects of Various Tail Arrangements on Wing-on and Wing-off Static Longitudinal and Lateral Stability Characteristics written by Robert W. Dunning and published by . This book was released on 1955 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Introduction to Aircraft Flight Mechanics by : Thomas R. Yechout
Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Book Synopsis Investigation of the Effects of Body Indentation and of Wing-plan-form Modification on the Longitudinal Characteristics of a 60 Degree Swept-wing Body Combination at Mach Numbers of 1.41, 1.61, and 2.01 by : John R. Jr Sevier
Download or read book Investigation of the Effects of Body Indentation and of Wing-plan-form Modification on the Longitudinal Characteristics of a 60 Degree Swept-wing Body Combination at Mach Numbers of 1.41, 1.61, and 2.01 written by John R. Jr Sevier and published by . This book was released on 1955 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Stability and Automatic Control by : Robert C. Nelson
Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Book Synopsis Static Stability Characteristics of a Winged Body with Various Inlet Configurations at Mach Numbers of 2, 5, 8, and 10 by : R. H. Burt
Download or read book Static Stability Characteristics of a Winged Body with Various Inlet Configurations at Mach Numbers of 2, 5, 8, and 10 written by R. H. Burt and published by . This book was released on 1964 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation has been conducted at Mach numbers of 2, 5, 8, and 10 to determine the static stability characteristics of a winged body configuration with various sizes and shapes of inlets attached. Selected results of the longitudinal stability and drag characteristics are presented for each configuration at the various mach numbers. The effect of inlet position along the model on the aerodynamic characteristics of two inlet configurations is presented for Mach numbers of 8 and 10. The investigation was performed at free-stream unit Reynolds numbers from 0.05 to 0.54 million per inch, angles of attack from -30 to 45 deg, and angles of yaw from 0 to 12 deg. (Author).
Book Synopsis Determination of Optimum Fin Planform and Airfoil Section for Minimizing Fin Hinge Moment by : Frederick K. Goodwin
Download or read book Determination of Optimum Fin Planform and Airfoil Section for Minimizing Fin Hinge Moment written by Frederick K. Goodwin and published by . This book was released on 1983 with total page 87 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second phase of an investigation of the hinge moments of all-movable controls as used on cruciform missiles is described. In the first phase, an attempt was made to develop a hinge-moment prediction method as general as possible for speeds ranging from subsonic to hypersonic. In that work, the method was successfully applied for Mach numbers ranging from 1.3 to 3.7. In the present phase of the investigation, the methods from phase one, with some modifications, have been used to develop a procedure for determining the optimum fin planform and airfoil section to minimize the fin hinge moment over a range of Mach numbers, angles of attack, and fin deflection angles. The Mach numbers range is restricted to supersonic. The transonic speed range cannot be handled since methods are not presently available for predicting the center-of-pressure shift due to thickness in this speed range. Experimental data are not available to assess the accuracy of the method at hypersonic speeds.
Download or read book Government Reports Index written by and published by . This book was released on 1974 with total page 1072 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 1974 with total page 1064 pages. Available in PDF, EPUB and Kindle. Book excerpt:
