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Effects of simplifying assumptions on optimal trajectory estimation for a high-performance aircraft

By Kern, Lura E.

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Book Id: WPLBN0002208135
Format Type: PDF eBook :
File Size: 0.9 MB
Reproduction Date: 2012

Title: Effects of simplifying assumptions on optimal trajectory estimation for a high-performance aircraft  
Author: Kern, Lura E.
Volume:
Language: English
Subject: AXIAL STRAIN, THERMAL RESISTANCE, ELASTOPLASTICITY
Collections: NASA Publication Collection
Historic
Publication Date:
1990
Publisher:

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E, K. L., L, D. E., & D, B. S. (1990). Effects of simplifying assumptions on optimal trajectory estimation for a high-performance aircraft. Retrieved from http://www.ebooklibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; When analyzing the performance of an aircraft, certain simplifying assumptions, which decrease the complexity of the problem, can often be m

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: AXIAL STRAIN; THERMAL RESISTANCE; ELASTOPLASTICITY; ELASTIC PROPERTIES; VISCOPLASTICITY; CREEP ANALYSIS; HYSTERESIS; COWLINGS; ENGINE INLETS; FINITE ELEMENT METHOD; HYPERSONIC INLETS; STRAIN DISTRIBUTION; STRESS DISTRIBUTION; STRESS-STRAIN RELATIONSHIPS

 

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