NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Explicit solution techniques for impact with contact constraintsModern military aircraft transparency systems, windshields and canopies, are complex systems which must meet a large and rapidly growing number of requirements. Many of these transparency system requirements are conflicting, presenting difficult balances which must be achieved. One example of a challenging requirements balance or trade is shaping for stealth versus aircrew vision. The large number of requirements involved may be grouped in a variety of areas including man-machine interface; structural integration with the airframe; combat hazards; environmental exposures; and supportability. Some individual requirements by themselves pose very difficult, severely nonlinear analysis problems. One such complex problem is that associated with the dynamic structural response resulting from high energy bird impact. An improved analytical capability for soft-body impact simulation was developed.
Document ID
19940014997
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mccarty, Robert E.
(Wright Lab. Wright-Patterson AFB, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1993
Publication Information
Publication: NASA. Langley Research Center, Computational Methods for Crashworthiness
Subject Category
Structural Mechanics
Accession Number
94N19470
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available