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

By Kern, Lura E.

Book Id: WPLBN0002208135
Format Type: PDF eBook:
File Size: 0.8 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:	Space and Aviation eDocuments Collection, NASA Publication Collection
Historic Publication Date:	1990
Publisher:


Citation APA MLA Chicago Lura E, B. K., L, D. E., & D, B. S. (1990). Effects of simplifying assumptions on optimal trajectory estimation for a high-performance aircraft. Retrieved from https://self.gutenberg.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