ISBN 9798672733258 is currently unpriced. Please contact us for pricing.
Available options are listed below:
Available options are listed below:
Stress Analysis of B-52B and B-52H Air-Launching Systems Failure-Critical Structural Components
AUTHOR | Administration (Nasa), National Aeronaut |
PUBLISHER | Independently Published (08/05/2020) |
PRODUCT TYPE | Paperback (Paperback) |
Description
The operational life analysis of any airborne failure-critical structural component requires the stress-load equation, which relates the applied load to the maximum tangential tensile stress at the critical stress point. The failure-critical structural components identified are the B-52B Pegasus pylon adapter shackles, B-52B Pegasus pylon hooks, B-52H airplane pylon hooks, B-52H airplane front fittings, B-52H airplane rear pylon fitting, and the B-52H airplane pylon lower sway brace. Finite-element stress analysis was performed on the said structural components, and the critical stress point was located and the stress-load equation was established for each failure-critical structural component. The ultimate load, yield load, and proof load needed for operational life analysis were established for each failure-critical structural component. Ko, William L. Armstrong Flight Research Center NASA/TP-2005-212862, H-2572 WU 761-90-00-SE-65 AIR LAUNCHING; B-52 AIRCRAFT; STRESS ANALYSIS; STRUCTURAL DESIGN; STRUCTURAL FAILURE; CRITICAL LOADING; FINITE ELEMENT METHOD; PYLONS; PEGASUS AIR-LAUNCHED BOOSTER; X-37 VEHICLE; SHEAR STRESS
Show More
Product Format
Product Details
ISBN-13:
9798672733258
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
40
Carton Quantity:
102
Product Dimensions:
8.50 x 0.08 x 11.02 inches
Weight:
0.26 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
The operational life analysis of any airborne failure-critical structural component requires the stress-load equation, which relates the applied load to the maximum tangential tensile stress at the critical stress point. The failure-critical structural components identified are the B-52B Pegasus pylon adapter shackles, B-52B Pegasus pylon hooks, B-52H airplane pylon hooks, B-52H airplane front fittings, B-52H airplane rear pylon fitting, and the B-52H airplane pylon lower sway brace. Finite-element stress analysis was performed on the said structural components, and the critical stress point was located and the stress-load equation was established for each failure-critical structural component. The ultimate load, yield load, and proof load needed for operational life analysis were established for each failure-critical structural component. Ko, William L. Armstrong Flight Research Center NASA/TP-2005-212862, H-2572 WU 761-90-00-SE-65 AIR LAUNCHING; B-52 AIRCRAFT; STRESS ANALYSIS; STRUCTURAL DESIGN; STRUCTURAL FAILURE; CRITICAL LOADING; FINITE ELEMENT METHOD; PYLONS; PEGASUS AIR-LAUNCHED BOOSTER; X-37 VEHICLE; SHEAR STRESS
Show More