Control Effectiveness And Tip Fin Dihedral Effects For The Hl 20 Lifting Body Configuration At Mach Numbers From 16 To 45

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Control Effectiveness and Tip-fin Dihedral Effects for the HL-20 Lifting-body Configuration at Mach Numbers from 1.6 to 4.5

Control Effectiveness and Tip-fin Dihedral Effects for the HL-20 Lifting-body Configuration at Mach Numbers from 1.6 to 4.5
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Total Pages : 96
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ISBN-10 : NASA:31769000523939
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Book Synopsis Control Effectiveness and Tip-fin Dihedral Effects for the HL-20 Lifting-body Configuration at Mach Numbers from 1.6 to 4.5 by : Christopher I. Cruz

Download or read book Control Effectiveness and Tip-fin Dihedral Effects for the HL-20 Lifting-body Configuration at Mach Numbers from 1.6 to 4.5 written by Christopher I. Cruz and published by . This book was released on 1995 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Control Effectiveness and Tip-fin Dihedral Effects for the HL-20 Lifting-body Configuration at Mach Numbers from 1.6 to 4.5 Related Books

Control Effectiveness and Tip-fin Dihedral Effects for the HL-20 Lifting-body Configuration at Mach Numbers from 1.6 to 4.5
Language: en
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Authors: Christopher I. Cruz
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Type: BOOK - Published: 1995 - Publisher:

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Control Effectiveness and Tip-Fin Dihedral Effects for the Hl-20 Lifting-Body Configuration at Mach Numbers from 1.6 to 4.5
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Wind tunnel tests were made with a scale model of the HL-20 in the Langley Unitary Plan Wind Tunnel. Pitch control was investigated by deflecting the elevon sur
Missile Aerodynamics
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The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions
Wingless Flight
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"Much has been written about the famous conflicts and battlegrounds of the East during the American Revolution. Perhaps less familiar, but equally important and
Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air
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A 0.0196-scale model of the HL-20 lifting body, one of several configurations proposed for future crewed spacecraft, was tested in the Langley 31-Inch Mach 10 T