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Aerodynamic Characteristics At Mach Numbers From 160 To 216 Of A Blunt Nose Missile Model Having A Triangular Cross Section And Fixed Triform Fins
Download Aerodynamic Characteristics At Mach Numbers From 160 To 216 Of A Blunt Nose Missile Model Having A Triangular Cross Section And Fixed Triform Fins full books in PDF, epub, and Kindle. Read online Aerodynamic Characteristics At Mach Numbers From 160 To 216 Of A Blunt Nose Missile Model Having A Triangular Cross Section And Fixed Triform Fins ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
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 Longitudinal Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.86 for a Fixed-span Missile with Three Wing Planforms by : M. Leroy Spearman
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.86 for a Fixed-span Missile with Three Wing Planforms written by M. Leroy Spearman and published by . This book was released on 1977 with total page 36 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 Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Maneuverable Missile with In-line Cruciform Wings and Canard Surfaces by : M. Leroy Spearman
Download or read book Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Maneuverable Missile with In-line Cruciform Wings and Canard Surfaces written by M. Leroy Spearman and published by . This book was released on 1967 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley Unitary Plan wind tunnel at Mach numbers from 1.50 to 4.63 to determine the aerodynamic characteristics of a maneuverable missile having in-line cruciform wings and canard surfaces oriented in 45° roll planes.
Book Synopsis Aerodynamic Characteristics at Mach Numbers of 3.95 and 4.63 for a Missile Model Having All-movable Wings and Interdigitated Tails by :
Download or read book Aerodynamic Characteristics at Mach Numbers of 3.95 and 4.63 for a Missile Model Having All-movable Wings and Interdigitated Tails written by and published by . This book was released on 1967 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 by : Earl D. Knechtel
Download or read book Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 written by Earl D. Knechtel and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.
Book Synopsis Normal Force, Center of Pressure, and Zero-lift Drag of Several Ballistic-type Missiles at Mach Numbers of 4.05 by : Edward F. Ulmann
Download or read book Normal Force, Center of Pressure, and Zero-lift Drag of Several Ballistic-type Missiles at Mach Numbers of 4.05 written by Edward F. Ulmann and published by . This book was released on 1954 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted at Mach number 4.05 to determine the aerodynamic characteristics of several missile models having turbulent boundary layers and to compare these results with available method of predicting the aerodynamic characteristics. (The condition of the boundary layer was determined by the china-clay-lacquer boundary-layer-visualization technique.) Normal force and pitching moment were measured through an angle-of-attack range of 0 to between 4 and 8 degrees, depending upon balance limitations, and at roll angles of 0 and 45 degrees; drag was measured only at 0 degrees angle of attack.
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 0.40 to 2.86 of a Missile Model Having All Movable Wings and Interdigitated Tails by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.40 to 2.86 of a Missile Model Having All Movable Wings and Interdigitated Tails written by and published by . This book was released on 1965 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 by : J. H. Jones
Download or read book Aerodynamic Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 written by J. H. Jones and published by . This book was released on 1972 with total page 220 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the Beech High Altitude Supersonic Target (HAST) missile.
Book Synopsis An Improved Semiempirical Method for Calculating Aerodynamics of Missiles with Noncircular Bodies by : Frankie Gale Moore
Download or read book An Improved Semiempirical Method for Calculating Aerodynamics of Missiles with Noncircular Bodies written by Frankie Gale Moore and published by . This book was released on 1997 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Aerodynamic Characteristics of a Model of a Rocket Missile with Several Arrangements of Folding Fins at Mach Numbers of 1.75, 2.15, 2.48, and 2.87 by :
Download or read book Investigation of the Aerodynamic Characteristics of a Model of a Rocket Missile with Several Arrangements of Folding Fins at Mach Numbers of 1.75, 2.15, 2.48, and 2.87 written by and published by . This book was released on 1960 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics and Flap Loads for a Blunt Pyramidal Configuration at Mach 5 and 8 by : William J. Evans
Download or read book Aerodynamic Characteristics and Flap Loads for a Blunt Pyramidal Configuration at Mach 5 and 8 written by William J. Evans and published by . This book was released on 1964 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt: Six-component force and moment data were obtained for Mach 5 and 8 flows over a blunt pyramidal configuration. The model had a triangular cross section and was composed of two dihedral surfaces and a 70-degree sweepback delta wing lower surface. Three-component force and moment data were obtained on a remotely controlled trailing edge flap at deflections up to 40 degrees. All three surfaces had trailing edge flaps and the model was tested with and without canards and a ventral fin. The model was pitched at angles of attack between ±54 degrees and side-slip angles between -4 and +14 degrees. For both Mach numbers, the data were obtained for a nominal free stream Reynolds number, based on model length, of 4.5 million. Selected configurations were tested at other Reynolds numbers between 1.2 and 9.1 million. (Author)
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 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 Experimental Aerodynamic Characteristics of a Fluidic-Controlled, Antitank Missile with Wraparound Fins at Mach Numbers from 0.2 to 3.0. Volume I. Data Report by : Troy A. Street
Download or read book Experimental Aerodynamic Characteristics of a Fluidic-Controlled, Antitank Missile with Wraparound Fins at Mach Numbers from 0.2 to 3.0. Volume I. Data Report written by Troy A. Street and published by . This book was released on 1971 with total page 105 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic wind tunnel tests have been conducted on an antitank missile model that contained stabilizing, wraparound fins and two different control systems. The model body had a 2-caliber secant ogive nose on an 8-caliber cylindrical segment. Two sets of fins were used with either a sonic (transverse) jet control system or the fluidic-control system interdigitated between the fins. The model angle of attack was varied from positive 6 degrees to negative 6 degrees for freestream Mach numbers from 0.2 to 3.0. The purpose of the test was to obtain information concerning the mutual aerodynamic interaction effect on the fin control system. Static force and moment data, at various angles of attack, and also body pressure data, in the vicinity of the control system, are presented. (Author).
Book Synopsis A Thesaurus of English Word Roots by : Horace Gerald Danner
Download or read book A Thesaurus of English Word Roots written by Horace Gerald Danner and published by Rowman & Littlefield. This book was released on 2014-03-27 with total page 1007 pages. Available in PDF, EPUB and Kindle. Book excerpt: Horace G. Danner’s A Thesaurus of English Word Roots is a compendium of the most-used word roots of the English language. As Timothy B. Noone notes in his foreword: “Dr. Danner’s book allows you not only to build up your passive English vocabulary, resulting in word recognition knowledge, but also gives you the rudiments for developing your active English vocabulary, making it possible to infer the meaning of words with which you are not yet acquainted. Your knowledge can now expand and will do so exponentially as your awareness of the roots in English words and your corresponding ability to decode unfamiliar words grows apace. This is the beginning of a fine mental linguistic library: so enjoy!” In A Thesaurus of English Word Roots, all word roots are listed alphabetically, along with the Greek or Latin words from which they derive, together with the roots’ original meanings. If the current meaning of an individual root differs from the original meaning, that is listed in a separate column. In the examples column, the words which contain the root are then listed, starting with their prefixes, for example, dysacousia, hyperacousia. These root-starting terms then are followed by terms where the root falls behind the word, e.g., acouesthesia and acoumeter. These words are followed by words where the root falls in the middle or the end, as in such terms as bradyacusia and odynacusis.. In this manner, A Thesaurus of English Word Roots places the word in as many word families as there are elements in the word. This work will interest linguists and philologists and anyone interested in the etymological aspects of English language.
