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Low-speed aerodynamic characteristics of a highly swept arrow wing configuration with several deflected leading edge concepts

By Gentry, G. L., Jr.

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Book Id: WPLBN0002205489
Format Type: PDF eBook :
File Size: 5.3 MB
Reproduction Date: 2012
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Title: Low-speed aerodynamic characteristics of a highly swept arrow wing configuration with several deflected leading edge concepts  
Author: Gentry, G. L., Jr.
Volume:
Language: English
Subject: COMPUTER PROGRAMS, ROLL, FLIGHT CONTROL
Collections: NASA Publication Collection
Historic
Publication Date:
1980
Publisher:

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L., Jr, G. G., & L., J, C. P. (1980). Low-speed aerodynamic characteristics of a highly swept arrow wing configuration with several deflected leading edge concepts. Retrieved from http://worldlibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; The effectiveness of leading edge concepts for minimizing or controlling leading edge flow separation was studied. Emphasis was placed on lo

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: COMPUTER PROGRAMS; ROLL; FLIGHT CONTROL; SPEED CONTROL; ROTATING BODIES; SEQUENCING; GUIDANCE (MOTION); SPACE SHUTTLE ORBITERS; SPACE TRANSPORTATION SYSTEM 1 FLIGHT; TERMINAL AREA ENERGY MANAGEMENT; AUTOMATIC PILOTS; BRAKES (FOR ARRESTING MOTION); GROUND TRACKS

 

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