Author: E. G Allee (Jr.)
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 44
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).
Store Separation Testing Techniques at the Arnold Engineering Development Center
Author: E. G Allee (Jr.)
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 44
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).
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 44
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).
Store Separation Testing Techniques at the Arnold Engineering Development Center
Author: J. P. Billingsley
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 96
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).
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 96
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).
Store Separation Testing Techniques at the Arnold Engineering Development Center
Author: J. B. Carman (Jr.)
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 92
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).
Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 92
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).
Store Separation
Author: Bertha M. Ryan
Publisher:
ISBN:
Category : Weapons systems
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Weapons systems
Languages : en
Pages : 82
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 312
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 312
Book Description
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048
Book Description
Captive Trajectory System for AEDC Supersonic Wind Tunnel (A) and Hypersonic Wind Tunnels (B) and (C)
Author: T. D. Buchanan
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 52
Book Description
In-flight Measurements of Captive Loads on a Store as Compared with Wind Tunnel and Mathematical Simulations
Author: A. R. Maddox
Publisher:
ISBN:
Category : Loads (Mechanics).
Languages : en
Pages : 46
Book Description
Publisher:
ISBN:
Category : Loads (Mechanics).
Languages : en
Pages : 46
Book Description
Technical Reports Awareness Circular : TRAC.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 746
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 746
Book Description
Database for Internal Store Carriage and Jettison
Author: R. E. Dix
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 212
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 212
Book Description