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Data Report For A Test Program To Study Transonic Flow Fields About Aircraft With Application To External Stores Volume Iii Mach Number 0975 Flow Field Survey Data For The 4 Percent Thick Wing Body Combination
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Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume III. Mach Number 0.975 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination 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 III. Mach Number 0.975 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 249 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. Volume III presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 0.975.
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume II. Mach Number 0.925 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination 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 II. Mach Number 0.925 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 249 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. Volume II, presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 0.925.
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume IV. Mach Number 1.025 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination 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 IV. Mach Number 1.025 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 248 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. Volume IV presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 1.025.
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume V. Flow-Field Survey Data for the 6-Percent Thick Wing-Body Combination 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 V. Flow-Field Survey Data for the 6-Percent Thick Wing-Body Combination written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 337 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. Volume V presents the tabulated flow-field data for 6-percent thick wing model.
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.
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume VI. 16T Wind Tunnel Tests 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 VI. 16T Wind Tunnel Tests written by Stanley C Perkins (Jr) and published by . This book was released on 1977 with total page 106 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. Volume VI presents data obtained for the 4-percent thick wing model in the 16T Wind Tunnel.
Book Synopsis Data Report for a Test Program to Study Transonic Flow Fields About Wing-Body/Pylon/Store Combinations. Volume II. Flow Field Survey Data for Configurations 21 and 22 by : S. S. Stahara
Download or read book Data Report for a Test Program to Study Transonic Flow Fields About Wing-Body/Pylon/Store Combinations. Volume II. Flow Field Survey Data for Configurations 21 and 22 written by S. S. Stahara and published by . This book was released on 1978 with total page 247 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume of the data report presents the flow-field survey data for configurations 21 and 22 at Mach numbers M1 = 0.925, M2 = 0.950, and M3 = 1.05 and angles of attack alpha = 0 deg, 2 deg, and 5 deg. The data were obtained in the 4T Wind Tunnel at Arnold Engineering and Development Center. The tests were performed at a nominal Reynolds number per foot of 3.0 million.
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 DARPA Technical Accomplishments by : Sidney G. Reed
Download or read book DARPA Technical Accomplishments written by Sidney G. Reed and published by . This book was released on 1990 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis New Approaches and Concepts in Turbulence by : T. Dracos
Download or read book New Approaches and Concepts in Turbulence written by T. Dracos and published by Springer Science & Business Media. This book was released on 1993-09-01 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book contains the proceedings of a colloquium held in Monte Verità from September 9-13, 1991. Special care has been taken to devote adequate space to the scientific discussions, which claimed about half of the time available. Scientists from all over the world presented their views on the importance of kinematic properties, topology and fractal geometry, and on the dynamic behaviour of turbulent flows. They debated the importance of coherent structures and the possibility to incorporate these in the statistical theory of turbulence, as well as their significance for the reduction of the degrees of freedom and the prospective of dynamical systems and chaos approaches to the problem of turbulence. Also under discussion was the relevance of these new approaches to the study of the instability and the origin of turbulence, and the importance of numerical and physical experiments in improving the understanding of turbulence.
Book Synopsis Predicting Water Availability in Irrigation Tank Cascade Systems by : C. J. Jayatilaka
Download or read book Predicting Water Availability in Irrigation Tank Cascade Systems written by C. J. Jayatilaka and published by IWMI. This book was released on 2001 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: Better water management in irrigation tank cascade systems is vital in achieving higher productive use of available water. To develop and implement management practices aimed at improving effective use of water, studies leading to the development of models that can predict available tank water in irrigation tank cascade systems are invaluable. This report presents a simple water balance model, Cascade, developed to predict tank water availability in the Thirappane tank cascade system in Anuradhapura, Sri Lanka. The report includes calibration of the model and its application to predict tank water availability for rice crops over a 10-year period.
Book Synopsis Flow Control by : Mohamed Gad-el-Hak
Download or read book Flow Control written by Mohamed Gad-el-Hak and published by Springer Science & Business Media. This book was released on 2003-07-01 with total page 533 pages. Available in PDF, EPUB and Kindle. Book excerpt: No be certain it can is not based mathematics. knowledge if upon da Vinci, (Leonardo 1452 1519) the humankind. Thinking is one greatest of Joys of Galilei, (Galileo 1564 1642) Now I think is to be the root all hydrodynamics and is at of physical science, second the to none in its mathematics. present beauty of Thomson (William (Lord Kelvin), 1824 1907) The book contains the lecture notes of of the nine instructors at present eight the short Flow Control: Fundamentals and which held course was Practices, in the week 24 28 June and Carg6se, Corsica, France, during 1996, repeated at the of Notre 9 13 1996. University Dame, Indiana, September Following the week in the course a on same was held. Corsica, 5 day workshop topic Selected from the scheduled to 1998 workshop are papers appear early special volume of the International Journal Heat Thermo of Experimental Transfer, and Fluid All Mechanics. three events were Jean Paul dynamics, organized by Bonnet of Universit6 de Andrew Pollard of Univer Poitiers, France, Queen's at and Mohamed Gad el Hak of the of sity Kingston, Canada, University Notre U.S.A.
Book Synopsis Reinventing the Propeller by : Jeremy R. Kinney
Download or read book Reinventing the Propeller written by Jeremy R. Kinney and published by Cambridge University Press. This book was released on 2017-03-24 with total page 391 pages. Available in PDF, EPUB and Kindle. Book excerpt: An international community of specialists reinvented the propeller during the Aeronautical Revolution, a vibrant period of innovation in North America and Europe from World War I to the end of World War II. They experienced both success and failure as they created competing designs that enabled increasingly sophisticated and 'modern' commercial and military aircraft to climb quicker and cruise faster using less power. Reinventing the Propeller nimbly moves from the minds of these inventors to their drawing boards, workshops, research and development facilities, and factories, and then shows us how their work performed in the air, both commercially and militarily. Reinventing the Propeller documents this story of a forgotten technology to reveal new perspectives on engineering, research and development, design, and the multi-layered social, cultural, financial, commercial, industrial, and military infrastructure of aviation.
Book Synopsis The Arecibo Antenna by : Helias Doundoulakis
Download or read book The Arecibo Antenna written by Helias Doundoulakis and published by Xlibris Corporation. This book was released on 2022-02-22 with total page 463 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Arecibo Radio Telescope (Arecibo) has made amazing findings that would otherwise have remained undiscovered. Yet, Arecibo’s inception is shrouded in mystery: unknown is the true story behind its creation, secret for all these years. Until now. In his final book, Helias Doundoulakis demystifies Arecibo for the novice, from dreams to drawings. The chronological account of the iconic telescope is made plain for all to see, which spanned six decades. Read how his brother, George Doundoulakis, undertook its conception and fielding, finally winning patent rights for his brother Helias, CIA director William Casey, and Gus Michalos. Follow the inseparable brothers on their journey of courage, inspiration, and brilliance that advanced the design of Arecibo and inspired generations of space scientists for years to come.
Book Synopsis Control of Fluid Flow by : Petros Koumoutsakos
Download or read book Control of Fluid Flow written by Petros Koumoutsakos and published by Springer Science & Business Media. This book was released on 2006-05-31 with total page 239 pages. Available in PDF, EPUB and Kindle. Book excerpt: This monograph presents the state of the art of theory and applications in fluid flow control, assembling contributions by leading experts in the field. The book covers a wide range of recent topics including vortex based control algorithms, incompressible turbulent boundary layers, aerodynamic flow control, control of mixing and reactive flow processes or nonlinear modeling and control of combustion dynamics.
Download or read book Waves in Flows written by Tomáš Bodnár and published by Springer Nature. This book was released on 2021-05-04 with total page 263 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume explores a range of recent advances in mathematical fluid mechanics, covering theoretical topics and numerical methods. Chapters are based on the lectures given at a workshop in the summer school Waves in Flows, held in Prague from August 27-31, 2018. A broad overview of cutting edge research is presented, with a focus on mathematical modeling and numerical simulations. Readers will find a thorough analysis of numerous state-of-the-art developments presented by leading experts in their respective fields. Specific topics covered include: Chemorepulsion Compressible Navier-Stokes systems Newtonian fluids Fluid-structure interactions Waves in Flows: The 2018 Prague-Sum Workshop Lectures will appeal to post-doctoral students and scientists whose work involves fluid mechanics.
Book Synopsis Introduction to Aeronautics by : Steven A. Brandt
Download or read book Introduction to Aeronautics written by Steven A. Brandt and published by AIAA. This book was released on 2004 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:
