Static Aerodynamic Characteristics Of A Series Of Generalized Slender Bodies With And Without Fins At Mach Numbers Form 06 To 30 And Angles Of Attack From 0 To 180 Deg PDF Download

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A Method for Estimating Static Aerodynamic Characteristics for Slender Bodies of Circular and Noncircular Cross Section Alone and with Lifting Surfaces at Angles of Attack from 0 ̊to 90 ̊

A Method for Estimating Static Aerodynamic Characteristics for Slender Bodies of Circular and Noncircular Cross Section Alone and with Lifting Surfaces at Angles of Attack from 0 ̊to 90 ̊
Author: Leland Howard Jorgensen
Publisher:
Total Pages: 44
Release: 1973
Genre: Aerodynamics
ISBN:
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Download A Method for Estimating Static Aerodynamic Characteristics for Slender Bodies of Circular and Noncircular Cross Section Alone and with Lifting Surfaces at Angles of Attack from 0 ̊to 90 ̊ Book in PDF, ePub and Kindle

An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations

An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations
Author: Harry W. Carlson
Publisher:
Total Pages: 36
Release: 1955
Genre: Aerodynamics
ISBN:
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Download An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations Book in PDF, ePub and Kindle

Abstract: An experimental investigation has been performed to determine the effect of changes in body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations. A series of 13 bodies having a given length and given longitudinal distribution of cross-sectional area but various cross-section shapes were tested at a Mach number of 2.01. The bodies were tested alone and in combination with a 47° sweptback wing having a 6-percent-thick hexagonal section.