Effect Of Fin Flare Combinations On The Aerodynamic Characteristics Of A Body At Mach Numbers 161 And 220

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Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20

Author	: Clyde Hayes
Publisher	:
Total Pages	: 44
Release	: 1965
ISBN-10	: UIUC:30112106868380
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20 by : Clyde Hayes

Download or read book Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20 written by Clyde Hayes and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20 Related Books

Language: en
Pages: 44

Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20

Authors: Clyde Hayes

Categories: Lift (Aerodynamics)

Type: BOOK - Published: 1965 - Publisher:

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Language: en
Pages: 38

Effect Opf Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20

Authors: Clyde Hayes

Categories:

Type: BOOK - Published: 1965 - Publisher:

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Language: en
Pages: 42

Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82

Authors: Ross B. Robinson

Categories: Mach number

Type: BOOK - Published: 1959 - Publisher:

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Language: en
Pages: 28

Some Effects of Fin Plan Form on the Static Stability of Fin-body Combinations at Mach Number 4.06

Authors: Edward F. Ulmann

Categories: Aerodynamics, Supersonic

Type: BOOK - Published: 1952 - Publisher:

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Language: en
Pages: 76

Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Variable-geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control

Authors: Roger H. Fournier

Categories: Space vehicles

Type: BOOK - Published: 1967 - Publisher:

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An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to det