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Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane

By Small, W. J.

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Book Id: WPLBN0002204577
Format Type: PDF eBook :
File Size: 1.8 MB
Reproduction Date: 2012

Title: Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane  
Author: Small, W. J.
Volume:
Language: English
Subject: ENGINE TESTS, NUCLEAR ENGINE FOR ROCKET VEHICLES, RADIATION EFFECTS
Collections: NASA Publication Collection
Historic
Publication Date:
1976
Publisher:

Citation

APA MLA Chicago

J, S. W., J, J. P., & P, W. J. (1976). Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane. Retrieved from http://www.worldlibrary.in/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Engine-nozzle airframe integration at hypersonic speeds was conducted by using a high-speed research aircraft concept as a focus. Recently d

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: ENGINE TESTS; NUCLEAR ENGINE FOR ROCKET VEHICLES; RADIATION EFFECTS; PROPULSION SYSTEM CONFIGURATIONS; REACTOR DESIGN; PROJECT PLANNING; RESEARCH MANAGEMENT

 

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