Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone Configuration at Mach Numbers from 2. 5 To 4. 5

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ISBN 13 : 9781731542083
Total Pages : 178 pages
Book Rating : 4.5/5 (42 download)

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Book Synopsis Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone Configuration at Mach Numbers from 2. 5 To 4. 5 by : National Aeronautics and Space Adm Nasa

Download or read book Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone Configuration at Mach Numbers from 2. 5 To 4. 5 written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-11-22 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was conducted to determine the longitudinal and lateral-directional aerodynamic characteristics of a generic wing-cone configuration at supersonic speeds. The fuselage has a 5 deg half-angle cone forebody, cylindrical midbody, and a 9 deg truncated cone afterbody. The delta wing (aspect ratio 1.0) had a 4 pct. thick diamond airfoil section. The tests were made in the Langley Unitary Plan Wind Tunnel at Mach numbers from 2.50 and 4.50. Angle of attack was varied from -4 to 28 degs, and angle of sideslip varied from -8 to 8 degs. Several configurations were studied to determine the effects of variations in wing longitudinal position, wing incidence, vertical tail configuration, canard shape, and nose bluntness. Typical effects of Reynolds number and Mach number on the longitudinal characteristics were observed. The incremental effects of the configuration variables were generally unaffected by Mach number. The directional stability characteristics of the large and small centerline mounted vertical tail configurations were significantly degraded with increasing angle of attack and Mach number. Covell, Peter F. and Walker, Ira J. and Howell, Dorothy T. Langley Research Center AERODYNAMIC CHARACTERISTICS; AERODYNAMIC CONFIGURATIONS; CANARD CONFIGURATIONS; DIRECTIONAL STABILITY; MACH NUMBER; REYNOLDS NUMBER; STABILIZERS (FLUID DYNAMICS); SUPERSONIC SPEED; WIND TUNNEL TESTS; AFTERBODIES; AIRFOIL PROFILES; ANGLE OF ATTACK; ASPECT RATIO; CYLINDRICAL BODIES; DELTA WINGS; FOREBODIES; FUSELAGES; SIDESLIP; TAIL ASSEMBLIES...

Longitudinal and Lateral-directional Aerodynamic Characteristics of a Wing-cone Configuration at Mach Numbers from 2.5 to 4.5

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ISBN 13 :
Total Pages : 180 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Longitudinal and Lateral-directional Aerodynamic Characteristics of a Wing-cone Configuration at Mach Numbers from 2.5 to 4.5 by : Peter F. Covell

Download or read book Longitudinal and Lateral-directional Aerodynamic Characteristics of a Wing-cone Configuration at Mach Numbers from 2.5 to 4.5 written by Peter F. Covell and published by . This book was released on 1992 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal and Lateral-directional Aerodynamic Characteristics of a Wing-cone Configuration at Mach Numbers from 2.5 to 4.5

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ISBN 13 :
Total Pages : pages
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Book Synopsis Longitudinal and Lateral-directional Aerodynamic Characteristics of a Wing-cone Configuration at Mach Numbers from 2.5 to 4.5 by : Peter F. Covell

Download or read book Longitudinal and Lateral-directional Aerodynamic Characteristics of a Wing-cone Configuration at Mach Numbers from 2.5 to 4.5 written by Peter F. Covell and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 by : George C. Kenyon

Download or read book The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 written by George C. Kenyon and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 4.63 for Two Variable-sweep Configurations

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 4.63 for Two Variable-sweep Configurations by :

Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 4.63 for Two Variable-sweep Configurations written by and published by . This book was released on 1965 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90 by :

Download or read book The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90 written by and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards by : A. Warner Robins

Download or read book Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards written by A. Warner Robins and published by . This book was released on 1979 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects by : Dal V. Maddalon

Download or read book Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects written by Dal V. Maddalon and published by . This book was released on 1966 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 340 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1992 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack

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ISBN 13 :
Total Pages : 104 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack by : James M. Luckring

Download or read book Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack written by James M. Luckring and published by . This book was released on 1977 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Wing Elevation, Incidence, and Camber on the Aerodynamic Characteristics of a Representative Hypersonic Cruise Configuration at Mach Numbers from 0.65 to 10.70

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ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Wing Elevation, Incidence, and Camber on the Aerodynamic Characteristics of a Representative Hypersonic Cruise Configuration at Mach Numbers from 0.65 to 10.70 by : Walter P. Nelms

Download or read book Effects of Wing Elevation, Incidence, and Camber on the Aerodynamic Characteristics of a Representative Hypersonic Cruise Configuration at Mach Numbers from 0.65 to 10.70 written by Walter P. Nelms and published by . This book was released on 1970 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 3.00, 3.96, and 4.65 of a Low-fineness-ratio Elliptical Hypersonic Configuration Having Variable-sweep Wing Panels

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 3.00, 3.96, and 4.65 of a Low-fineness-ratio Elliptical Hypersonic Configuration Having Variable-sweep Wing Panels by :

Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 3.00, 3.96, and 4.65 of a Low-fineness-ratio Elliptical Hypersonic Configuration Having Variable-sweep Wing Panels written by and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing by : Harry W. Carlson

Download or read book Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing written by Harry W. Carlson and published by . This book was released on 1963 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90

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ISBN 13 :
Total Pages : 49 pages
Book Rating : 4.:/5 (76 download)

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Book Synopsis The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 by : George C. Kenyon

Download or read book The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 written by George C. Kenyon and published by . This book was released on 1961 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 320 pages
Book Rating : 4.:/5 (3 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 776 pages
Book Rating : 4.:/5 (26 download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1971 with total page 776 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 390 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1966 with total page 390 pages. Available in PDF, EPUB and Kindle. Book excerpt: