Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63

Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63
Title Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 PDF eBook
Author James F. Campbell
Publisher
Pages 44
Release 1967
Genre Aerodynamics
ISBN

Download Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 Book in PDF, Epub and Kindle

Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63

Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63
Title Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 PDF eBook
Author James F. Campbell
Publisher
Pages 32
Release 1967
Genre
ISBN

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Longitudinal Aerodynamic Performance of a Series of Power-law and Minimum-wave-drag Bodies at Mach 6 and Several Reynolds Numbers

Longitudinal Aerodynamic Performance of a Series of Power-law and Minimum-wave-drag Bodies at Mach 6 and Several Reynolds Numbers
Title Longitudinal Aerodynamic Performance of a Series of Power-law and Minimum-wave-drag Bodies at Mach 6 and Several Reynolds Numbers PDF eBook
Author George C. Ashby
Publisher
Pages 36
Release 1974
Genre Aerodynamics, Hypersonic
ISBN

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Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing

Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing
Title Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing PDF eBook
Author Edward J. Ray
Publisher
Pages 84
Release 1967
Genre
ISBN

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STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG

STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG
Title STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG PDF eBook
Author
Publisher
Pages 48
Release 1959
Genre
ISBN

Download STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG 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
Title 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 PDF eBook
Author Harry W. Carlson
Publisher
Pages 36
Release 1955
Genre Aerodynamics
ISBN

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.

The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93

The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93
Title The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93 PDF eBook
Author W. P. Henderson
Publisher
Pages 26
Release 1960
Genre
ISBN

Download The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93 Book in PDF, Epub and Kindle