Aircraft Crash Survival Design Guide. Volume 3. Aircraft Structural Crash Resistance
Abstract
This five volume publication has been compiled to assist design engineers in understanding the design considerations associated with the development of crash resistant U.S. Army aircraft. A collection of available information and data pertinent to aircraft crash resistance is presented, along with suggested design conditions and criteria. The five volumes of the Aircraft Crash Survival Design Guide cover the following topics: Volume I - Design Criteria and Checklists; Volume II - Aircraft Design Crash Impact Conditions and Human Tolerance; Volume III - Aircraft Structural Crash Resistance; Volume IV - Aircraft Seats, Restraints, Litters and Cockpit/Cabin Delethalization; and Volume V - Aircraft Postcrash Survival. This volume (Volume III) contains information on the design of aircraft structures and structural elements for improved crash survivability. Current requirements for structural design of U.S. Army aircraft pertaining to crash resistance are discussed. Principles for crash-resistant design are presented in detail for the landing gear and fuselage subject to a range of crash conditions, including impacts that are primarily longitudinal, vertical or lateral in nature and those that involve more complicated dynamic conditions, such as rollover. Analytical methods for evaluating structural crash resistance are described.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1989
- Accession Number
- ADA218436
Entities
People
- Akif O. Bolukbasi
- Alan D. Lane
- James C. Warrick
- Norman A. Merritt
- Richard E. Zimmerman