Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Investigation Of The Aerodynamic Characteristics Of Two Preliminary Designs Of Scout Research Vehicle At Mach Numbers From 177 To 465
Download Investigation Of The Aerodynamic Characteristics Of Two Preliminary Designs Of Scout Research Vehicle At Mach Numbers From 177 To 465 full books in PDF, epub, and Kindle. Read online Investigation Of The Aerodynamic Characteristics Of Two Preliminary Designs Of Scout Research Vehicle At Mach Numbers From 177 To 465 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Investigation of the Aerodynamic Characteristics of Two Preliminary Designs of Scout Research Vehicle at Mach Numbers from 1.77 to 4.65 by : Robert J. Keynton
Download or read book Investigation of the Aerodynamic Characteristics of Two Preliminary Designs of Scout Research Vehicle at Mach Numbers from 1.77 to 4.65 written by Robert J. Keynton and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle by : Byron M. Jaquet
Download or read book Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle written by Byron M. Jaquet and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Loading Characteristics of a 1/10-scale Model of the Three-stage Scout Vehicle at Mach Numbers 1.57 to 4.65 by : Lloyd S. Jernell
Download or read book Aerodynamic Loading Characteristics of a 1/10-scale Model of the Three-stage Scout Vehicle at Mach Numbers 1.57 to 4.65 written by Lloyd S. Jernell and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 by : James F. Campbell
Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Configurations of the Scout Vehicle and of a Number of Related Models by : Thomas C. Kelly
Download or read book Transonic Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Configurations of the Scout Vehicle and of a Number of Related Models written by Thomas C. Kelly and published by . This book was released on 1961 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results have been obtained i n t h e Langley 8-foot transonic pressure tunnel at Mach numbers from 0.40 t o 1.20 for several configurations of the Scout vehicle and f o r a number of related models. Tests extended over an angle-of-attack range from about -10 degrees to 10 degrees at a Reynolds number per foot of about 3.8 x 10 sup 6.
Book Synopsis Aerodynamic Characteristics in Pitch and Sideslip of a 1/15-scale Model of the Scout Vehicle at a Mach Number of 2.01 by : Ross B. Robinson
Download or read book Aerodynamic Characteristics in Pitch and Sideslip of a 1/15-scale Model of the Scout Vehicle at a Mach Number of 2.01 written by Ross B. Robinson and published by . This book was released on 1961 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1/10-scale Model of the Blue Scout Jr. at Mach Numbers from 0.40 to 1.03 by : Thomas C. Kelly
Download or read book Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1/10-scale Model of the Blue Scout Jr. at Mach Numbers from 0.40 to 1.03 written by Thomas C. Kelly and published by . This book was released on 1962 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Exploratory Investigation of the Aerodynamic Characteristics of a Biwing Vehicle at Mach 20.3 by : Peter T. Bernot
Download or read book Exploratory Investigation of the Aerodynamic Characteristics of a Biwing Vehicle at Mach 20.3 written by Peter T. Bernot and published by . This book was released on 1985 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing by : Edward J. Ray
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Exploratory Investigation of the Aerodynamic Characteristics of a Biwing Vehicle at Mach 20.3 by :
Download or read book Exploratory Investigation of the Aerodynamic Characteristics of a Biwing Vehicle at Mach 20.3 written by and published by . This book was released on 1984 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors by : Dennis E. Fuller
Download or read book Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors written by Dennis E. Fuller and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic and Flow-visualization Studies of Two Delta-wing Entry Vehicles at a Mach Number of 20.3 by : James P. Arrington
Download or read book Aerodynamic and Flow-visualization Studies of Two Delta-wing Entry Vehicles at a Mach Number of 20.3 written by James P. Arrington and published by . This book was released on 1973 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: The longitudinal, lateral, and directional aerodynamic characteristics of two space shuttle concepts have been obtained in helium for operational flight Reynolds numbers at angles of attack from minus 10 to 55 deg. Included are elevon control deflections, roll control due to ailerons, and the effects of a nose modification. Selected results were compared with those derived from tangent-cone and Newtonian theories. Also included are results of a flow-visualization study consisting of electron-beam-illuminated flow and surface oil-flow patterns.
Book Synopsis Aerodynamic Characteristics of Two Single-stage-to-orbit Vehicles at Mach 20.3 by : Peter T. Bernot
Download or read book Aerodynamic Characteristics of Two Single-stage-to-orbit Vehicles at Mach 20.3 written by Peter T. Bernot and published by . This book was released on 1977 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Off-design Aerodynamic Characteristics at Mach Numbers 1.61 and 2.20 of a Series of Highly Swept Arrow Wings Designed for Mach Number 2.0 Employing Various Degrees of Twist and Camber by : Wilbur D. Middleton
Download or read book Off-design Aerodynamic Characteristics at Mach Numbers 1.61 and 2.20 of a Series of Highly Swept Arrow Wings Designed for Mach Number 2.0 Employing Various Degrees of Twist and Camber written by Wilbur D. Middleton and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 by : James C. Ellison
Download or read book Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 written by James C. Ellison and published by . This book was released on 1971 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Also available online.
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:
Book Synopsis Facing the Heat Barrier by : T. A. Heppenheimer
Download or read book Facing the Heat Barrier written by T. A. Heppenheimer and published by . This book was released on 2006 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hypersonics is the study of flight at speeds where aerodynamic heating dominates the physics of the problem. Typically this is Mach 5 and higher. Hypersonics is an engineering science with close links to supersonics and engine design. Within this field, many of the most important results have been experimental. The principal facilities have been wind tunnels and related devices, which have produced flows with speeds up to orbital velocity. Why is it important? Hypersonics has had two major applications. The first has been to provide thermal protection during atmospheric entry. Success in this enterprise has supported ballistic-missile nose cones, has returned strategic reconnaissance photos from orbit and astronauts from the Moon, and has even dropped an instrument package into the atmosphere of Jupiter. The last of these approached Jupiter at four times the speed of a lunar mission returning to Earth. Work with re-entry has advanced rapidly because of its obvious importance. The second application has involved high-speed propulsion and has sought to develop the scramjet as an advanced airbreathing ramjet. Scramjets are built to run cool and thereby to achieve near-orbital speeds. They were important during the Strategic Defense Initiative, when a set of these engines was to power the experimental X-30 as a major new launch vehicle. This effort fell short, but the X-43A, carrying a scramjet, has recently flown at Mach 9.65 by using a rocket. Atmospheric entry today is fully mature as an engineering discipline. Still, the Jupiter experience shows that work with its applications continues to reach for new achievements. Studies of scramjets, by contrast, still seek full success, in which such engines can accelerate a vehicle without the use of rockets. Hence, there is much to do in this area as well. For instance, work with computers may soon show just how good scramjets can become. NASA SP-2007-4232
