Store Separation Testing Techniques at the Arnold Engineering Development Center PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Store Separation Testing Techniques at the Arnold Engineering Development Center PDF full book. Access full book title Store Separation Testing Techniques at the Arnold Engineering Development Center by E. G Allee (Jr.). Download full books in PDF and EPUB format.
Author: E. G Allee (Jr.)
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 44
Get Book Here
Book Description
Dynamic drop testing is a method of trajectory simulation whereby store models which are both geometrically and dynamically scaled are released in the wind tunnel air stream and the resulting trajectories are mapped photographically. Drop testing is often used when captive trajectory testing is not feasible or for final trajectory verification prior to flight tests. (Author).
Author: E. G Allee (Jr.)
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 44
Get Book Here
Book Description
Dynamic drop testing is a method of trajectory simulation whereby store models which are both geometrically and dynamically scaled are released in the wind tunnel air stream and the resulting trajectories are mapped photographically. Drop testing is often used when captive trajectory testing is not feasible or for final trajectory verification prior to flight tests. (Author).
Author: J. P. Billingsley
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 96
Get Book Here
Book Description
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).
Author: J. B. Carman (Jr.)
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 92
Get Book Here
Book Description
The purpose of this report is to describe the formulation and basic composition of several store separation techniques (dynamic drop, wind tunnel computer simulation, and analytical computer simulation) along with the benefits and limitations of each. In the course of the report, guidelines are established for use in formulation of future store separation test and evaluation programs. (Author).
Author: Bertha M. Ryan
Publisher:
ISBN:
Category : Weapons systems
Languages : en
Pages : 82
Get Book Here
Book Description
Author: Stephen C. Korn
Publisher:
ISBN:
Category : Bomb racks
Languages : en
Pages : 272
Get Book Here
Book Description
This report documents the external flow fields caused by various weapon configurations on the wing of an F-4 aircraft, verifies assumptions made in the flow angularity technique, and presents the documentation for the 'Flow Angularity Computer Program' with example trajectories. The flow angularity program is presently capable of calculating the trajectories of stores off the inboard and outboard wing stations in either single, triple ejector rack, or multiple ejector rack configurations. The assumptions made in the flow angularity technique have been analyzed and generally validated as good approximations. (Author).
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 312
Get Book Here
Book Description
Author: T. D. Buchanan
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 52
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 746
Get Book Here
Book Description
Author: R. E. Dix
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 212
Get Book Here
Book Description
