Influences of Sway Braces and Mounting Gaps on the Static Aerodynamic Loading of External Stores

Influences of Sway Braces and Mounting Gaps on the Static Aerodynamic Loading of External Stores PDF Author: R. E. Dix
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 140

Get Book Here

Book Description
As the scale factor applied in the design of wind tunnel models is reduced, many details of the configuration being simulated are customarily omitted. A series of experiments was conducted in the Aerodynamic Wind Tunnel (4T) of the Propulsion Wind Tunnel Facility at the Arnold Engineering Development Center to evaluate the effect on captive store loading of model details such as sway braces and mounting gaps existing between store and aircraft components. Six components of aerodynamic loads acting on both pylon- and rack-mounted stores in the captive position were measured, a limited number of store separation trajectories was predicted using the captive trajectory system, and a brief comparison of wind tunnel and in-flight measurements of captive loads was made. It was determined that the effects of mounting gaps or flow ventilation passages were generally small, but that sway braces can significantly influence both captive loads and separation trajectories. It was also observed that better agreement between wind tunnel and in-flight measurements of captive store loading resulted when mounting gaps and sway braces were simulated on the wind-tunnel models. (Author).

Influences of Sway Braces and Mounting Gaps on the Static Aerodynamic Loading of External Stores

Influences of Sway Braces and Mounting Gaps on the Static Aerodynamic Loading of External Stores PDF Author: R. E. Dix
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 140

Get Book Here

Book Description
As the scale factor applied in the design of wind tunnel models is reduced, many details of the configuration being simulated are customarily omitted. A series of experiments was conducted in the Aerodynamic Wind Tunnel (4T) of the Propulsion Wind Tunnel Facility at the Arnold Engineering Development Center to evaluate the effect on captive store loading of model details such as sway braces and mounting gaps existing between store and aircraft components. Six components of aerodynamic loads acting on both pylon- and rack-mounted stores in the captive position were measured, a limited number of store separation trajectories was predicted using the captive trajectory system, and a brief comparison of wind tunnel and in-flight measurements of captive loads was made. It was determined that the effects of mounting gaps or flow ventilation passages were generally small, but that sway braces can significantly influence both captive loads and separation trajectories. It was also observed that better agreement between wind tunnel and in-flight measurements of captive store loading resulted when mounting gaps and sway braces were simulated on the wind-tunnel models. (Author).

Influences of Sway Braces and Mounting Gaps on the Static Aerodynamic Loading of External Stores

Influences of Sway Braces and Mounting Gaps on the Static Aerodynamic Loading of External Stores PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

Get Book Here

Book Description
As the scale factor applied in the design of wind tunnel models is reduced, many details of the configuration being simulated are customarily omitted. A series of experiments was conducted in the Aerodynamic Wind Tunnel (4T) of the Propulsion Wind Tunnel Facility at the Arnold Engineering Development Center to evaluate the effect on captive store loading of model details such as sway braces and mounting gaps existing between store and aircraft components. Six components of aerodynamic loads acting on both pylon- and rack-mounted stores in the captive position were measured, a limited number of store separation trajectories was predicted using the captive trajectory system, and a brief comparison of wind tunnel and in-flight measurements of captive loads was made. It was determined that the effects of mounting gaps or flow ventilation passages were generally small, but that sway braces can significantly influence both captive loads and separation trajectories. It was also observed that better agreement between wind tunnel and in-flight measurements of captive store loading resulted when mounting gaps and sway braces were simulated on the wind-tunnel models. (Author).

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 272

Get Book Here

Book Description


In-flight Measurements of Captive Loads on a Store as Compared with Wind Tunnel and Mathematical Simulations

In-flight Measurements of Captive Loads on a Store as Compared with Wind Tunnel and Mathematical Simulations PDF Author: A. R. Maddox
Publisher:
ISBN:
Category : Loads (Mechanics).
Languages : en
Pages : 46

Get Book Here

Book Description


Comparison of Wind Tunnel and Flight Test Measurements of Static Aerodynamic Loading of a Captive Store

Comparison of Wind Tunnel and Flight Test Measurements of Static Aerodynamic Loading of a Captive Store PDF Author: R. E. Dix
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 122

Get Book Here

Book Description


NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 720

Get Book Here

Book Description


Store Separation Testing Techniques at the Arnold Engineering Development Center

Store Separation Testing Techniques at the Arnold Engineering Development Center PDF 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).

Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 708

Get Book Here

Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

A Source-Doublet Approach to Modeling Triple Ejector Rack Store Configurations and Force Calculations

A Source-Doublet Approach to Modeling Triple Ejector Rack Store Configurations and Force Calculations PDF Author: Calvin L. Dyer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 96

Get Book Here

Book Description


Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1126

Get Book Here

Book Description