Store Separation Testing Techniques At The Arnold Engineering Development Center Volume 2 Description Of Captive Trajectory Store Separation Testing In The Aerodynamic Wind Tunnel 4t
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Store Separation Testing Techniques At The Arnold Engineering Development Center
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Author : J. B. Carman (Jr.)
language : en
Publisher:
Release Date : 1980
Store Separation Testing Techniques At The Arnold Engineering Development Center written by J. B. Carman (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Airplanes, Military categories.
This report describes the current captive trajectory support (CTS) hardware, system operation, and the captive trajectory applications program for the Aerodynamic Wind Tunnel (4T). Also included are brief descriptions of additional CTS applications and some guidelines for potential users of the system.
Store Separation Testing Techniques At The Arnold Engineering Development Center
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Author : J. P. Billingsley
language : en
Publisher:
Release Date : 1979
Store Separation Testing Techniques At The Arnold Engineering Development Center written by J. P. Billingsley and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Airplanes, Military categories.
Tests were conducted on a four-finned, ogive-cylinder store model which was mounted on the von Karman Gas Dynamics Facility (VKF) Captive Trajectory System (CTS) in the Arnold Engineering Development Center (AEDC) Supersonic Wind Tunnel A. The purpose of these tests was to provide information necessary for an independent check on the VKF CTS trajectory mode results. Grid and trajectory data were obtained for the store, both in the free stream and in the interference flow field of a generalized parent-aircraft model. The Mach number was 1.63, with Reynolds numbers per foot of 5.0 and 3.8 million. Grid data from these tests were used in conjunction with the Air Force Flight Dynamics Laboratory (AFFDL) Six-Degree-of-Freedom Computer Program (SDFCP) to simulate the trajectories obtained by the VKF CTS. These SDFCP simulations compared favorably with the CTS trajectories, providing an important compared favorably with the CTS trajectories, providing an important independent verification of the VKF CTS trajectory mode results. This report documents this validation effort and provides a general description of the VKF CTS as well as guidelines for potential users of this system. (Author).
Captive Trajectory System For Aedc Supersonic Wind Tunnel A And Hypersonic Wind Tunnels B And C
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Author : T. D. Buchanan
language : en
Publisher:
Release Date : 1983
Captive Trajectory System For Aedc Supersonic Wind Tunnel A And Hypersonic Wind Tunnels B And C written by T. D. Buchanan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with Hypersonic wind tunnels categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1980
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aeronautics categories.
Technical Abstract Bulletin
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Author :
language : en
Publisher:
Release Date : 1979
Technical Abstract Bulletin written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Science categories.
Cavity Aeroacoustics
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Author : Richard E. Dix
language : en
Publisher:
Release Date : 1990
Cavity Aeroacoustics written by Richard E. Dix and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Aeroacoustics categories.
An Analytic Investigation Of Accuracy Requirements For Onboard Instrumentation And Film Data For Dynamically Scaled Wind Tunnel Drop Models
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Author : K. S. Keen
language : en
Publisher:
Release Date : 1997
An Analytic Investigation Of Accuracy Requirements For Onboard Instrumentation And Film Data For Dynamically Scaled Wind Tunnel Drop Models written by K. S. Keen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with Equations of motion categories.
An analytic study was conducted to evaluate anticipated ranges and required accuracies for onboard linear acceleration and angular rate (or acceleration) measurement equipment to be mounted within dynamically scaled wind tunnel drop models. Generic simulations of the separation motion of a tumbling fuel tank both at full scale and at 1/15th wind tunnel model scale were generated using an analytic trajectory simulation program coupled with a prescribed aerodynamic database. The simulations provide a basis for sizing the required instrumentation for proof of concept demonstrations of telemetry techniques in the wind tunnel. The simulations were also used as test cases to demonstrate extraction of aerodynamic information from drop data positions and orientations as read from film records via an inverse solution of the store equations of motion. The studies also aid identification and evaluation of inaccuracies associated with the basic dynamic scaling laws and standard film based data reduction techniques.
Experimental And Theoretical Study Of Cavity Acoustics
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Author : R. E. Dix
language : en
Publisher:
Release Date : 2000
Experimental And Theoretical Study Of Cavity Acoustics written by R. E. Dix and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Aeroacoustics categories.
Between 1986 and 1990, a large database was compiled at AEDC from the results of a series of wind tunnel experiments investigating the aerodynamics of flow over open cavities. The database, known as the Weapons Internal Carriage and Separation (WICS) database, covered four experiments that were completed in the AEDC wind tunnels. The initial database documentation focused on the test and data, but included very little analysis of the results. The purpose of the present work is to report analysis of the cavity acoustics and trajectory data. In addition, an updated engineering mathematical model for cavity aeroacoustics is presented.
Database For Internal Store Carriage And Jettison
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Author : R. E. Dix
language : en
Publisher:
Release Date : 1990
Database For Internal Store Carriage And Jettison written by R. E. Dix and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Aerodynamic load categories.
18th Aiaa Aerospace Ground Testing Conference
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Author :
language : en
Publisher:
Release Date : 1994
18th Aiaa Aerospace Ground Testing Conference written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aerodynamics categories.