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Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 deg delta wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70

By Bond, A. C.

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Book Id: WPLBN0002200167
Format Type: PDF eBook :
File Size: 2.4 MB
Reproduction Date: 2012
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Title: Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 deg delta wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70  
Author: Bond, A. C.
Volume:
Language: English
Subject: CATALYTIC ACTIVITY, HYDROGEN OXYGEN ENGINES, IGNITION
Collections: NASA Publication Collection
Historic
Publication Date:
1954
Publisher:

Citation

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C, B. A., & G, S. A. (1954). Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 deg delta wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70. Retrieved from http://netlibrary.net/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents

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: CATALYTIC ACTIVITY; HYDROGEN OXYGEN ENGINES; IGNITION; CATALYSTS; METAL OXIDES; NOBLE METALS; LIQUID HYDROGEN; LIQUID OXYGEN

 

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