AERODYNAMIC CHARACTERISTICS OF TWO RECTANGULAR-PLAN-FORM, ALLMOVABLE CONTROLS IN COMBINATION WITH A SLENDER BODY OF REVOLUTION AT MACH NUMBERS FROM 3.00 TO 6.25

By Gloria, H. R.

Book Id: WPLBN0002196616
Format Type: PDF eBook :
File Size:
Reproduction Date: 2012

Title:	AERODYNAMIC CHARACTERISTICS OF TWO RECTANGULAR-PLAN-FORM, ALLMOVABLE CONTROLS IN COMBINATION WITH A SLENDER BODY OF REVOLUTION AT MACH NUMBERS FROM 3.00 TO 6.25
Author:	Gloria, H. R.
Volume:
Language:	English
Subject:	AERODYNAMIC CHARACTERISTICS, AERODYNAMIC CHARACTERISTICS, SLENDER BODY
Collections:	NASA Publication Collection
Historic Publication Date:	20451
Publisher:


Citation APA MLA Chicago R, G. H., & J, W. T. (20451). AERODYNAMIC CHARACTERISTICS OF TWO RECTANGULAR-PLAN-FORM, ALLMOVABLE CONTROLS IN COMBINATION WITH A SLENDER BODY OF REVOLUTION AT MACH NUMBERS FROM 3.00 TO 6.25. Retrieved from http://self.gutenberg.org/

Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Aerodynamic characteristics of rectangular planform, all-movable controls combined with slender body of revolution at mach 3 to 6.25

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: AERODYNAMIC CHARACTERISTICS; AERODYNAMIC CHARACTERISTICS; SLENDER BODY; RECTANGULAR PLANFORM; BODY OF REVOLUTION; CONTROL SURFACE; ANGLE OF ATTACK; BODIES OF REVOLUTION; CONTROL SURFACES; HIGH SPEED; MACH NUMBER; RECTANGULAR PLANFORMS; SLENDER BODIES; SUPERSONIC SPEED