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Flow Field Measurements Around An Ogive Cylinder At Angles Of Attack Up To 15 Degrees For Mach Numbers 35 And 4
Download Flow Field Measurements Around An Ogive Cylinder At Angles Of Attack Up To 15 Degrees For Mach Numbers 35 And 4 full books in PDF, epub, and Kindle. Read online Flow Field Measurements Around An Ogive Cylinder At Angles Of Attack Up To 15 Degrees For Mach Numbers 35 And 4 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Flow Field Measurements Around an Ogive-cylinder at Angles of Attack Up to 15 Degrees for Mach Numbers 3.5 and 4 by : William C. Ragsdale
Download or read book Flow Field Measurements Around an Ogive-cylinder at Angles of Attack Up to 15 Degrees for Mach Numbers 3.5 and 4 written by William C. Ragsdale and published by . This book was released on 1972 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt: The flow field was surveyed at one station (X/D = 6.5) on an ogive- cylinder having a tangent ogive nose with a fineness ratio of 4. The surveys were performed with pitot tubes and cone pressure probes at angles of attack of 0, 5, 10 and 15 degrees for Mach numbers 3.52 and 4.07. Surface static pressures were also measured. The results of the tests are presented in tabular and plotted form. Comparisons are made with inviscid flow fields calculations and with experimental results from other investigations.
Book Synopsis Three-dimensional Interactions and Vortical Flows with Emphasis on High Speeds by : David J. Peake
Download or read book Three-dimensional Interactions and Vortical Flows with Emphasis on High Speeds written by David J. Peake and published by . This book was released on 1980 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1976 with total page 1072 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2.46 by : Frank J. Centolanzi
Download or read book Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2.46 written by Frank J. Centolanzi and published by . This book was released on 1959 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Collection of Technical Papers by :
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1977 with total page 846 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of Flow Properties in the Vicinity of Three Wing-fuselage Combinations at Mach Numbers of 1.61 and 2.01 by : Harry W. Carlson
Download or read book Measurements of Flow Properties in the Vicinity of Three Wing-fuselage Combinations at Mach Numbers of 1.61 and 2.01 written by Harry W. Carlson and published by . This book was released on 1959 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° by : Leroy Devan
Download or read book Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° written by Leroy Devan and published by . This book was released on 1980 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Three-dimensional Flows about Simple Components at Angle of Attack by : David J. Peake
Download or read book Three-dimensional Flows about Simple Components at Angle of Attack written by David J. Peake and published by . This book was released on 1982 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The AFFDL-Nielsen Flow-field Study by : William T Strike (Jr.)
Download or read book The AFFDL-Nielsen Flow-field Study written by William T Strike (Jr.) and published by . This book was released on 1976 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: This test was conducted in support of a program to develop a generalized analytical method for predicting the separation characteristics of stores from a high-speed aircraft (parent body). The tests were conducted in the von Karman Gas Dynamics Facility (VKF), Tunnel A, at nominal Mach numbers of 1.5, 1.76, 2.0, and 2.5 at a nominal free-stream Reynolds number of 4 x 10 to 6th power per foot. The test program involved three phases, namely flow-field surveys using a cone probe rake to determine local flow-field angles and velocity, pressure distributions on the store as it separated from a parent body, and six-component force and moment data on the store. The tests were conducted at angles of attack of zero and five degrees. This document contains a detailed description of the calibration procedure for the 20-deg half-angle cone probes and the method used to evaluate the local flow-field properties from the cone probe surface pressure and pitot pressure measurements. Also included is a comparison of integrated pressure data with the force and moment data obtained on the storebody by a balance. (Author).
Book Synopsis Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2.46 by : Frank J. Centolanzi
Download or read book Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2.46 written by Frank J. Centolanzi and published by . This book was released on 1959 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1991 with total page 1270 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Nine Ogive-Cylinder-Flare Configurations at Mach Numbers of 1.1 to 4.5 by : James Robert Burt (Jr)
Download or read book Aerodynamic Characteristics of Nine Ogive-Cylinder-Flare Configurations at Mach Numbers of 1.1 to 4.5 written by James Robert Burt (Jr) and published by . This book was released on 1970 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of normal force, center of pressure, and axial force on nine ogive-cylinder-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 varied from about -4.5 to 6.5 degrees. The effects of Mach number, flare length, and flare diameter on model normal force, center of pressure, and axial force are shown. (Author).
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1998 with total page 980 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44 by :
Download or read book Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44 written by and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements by :
Download or read book Government Reports Announcements written by and published by . This book was released on 1973 with total page 932 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 908 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume I. Summary Report, Tunnel-Empty and Mach-Number Survey Data, Force and Moment Data, and Pressure Data by : Stanley C Perkins (Jr)
Download or read book Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume I. Summary Report, Tunnel-Empty and Mach-Number Survey Data, Force and Moment Data, and Pressure Data written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Flow velocities and static pressures were also measured near the tunnel walls to provide outer flow field information. This report presents the data obtained during the test program conducted in the 4T and 16T Wind Tunnels at Arnold Engineering Development Center. The Flow-field data were obtained at Mach numbers 0.925, 0.975, and 1.025 and constitute the major part of the data. Volume I is a summary report which gives detailed information on the test program and presents uncertainties associated with the various types of data taken in the 4T Wind Tunnel. The volume also presents tunnel-empty and Mach-number surveys, as well as tabulated force and moment and pressure data for the Mach number range 0.80 to 1.15 and angles of attack -2, -5, 0, 2, and 5.
