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Longitudinal Aerodynamic Characteristics Of Two Blunted Cone Reentry Configurations At Mach Numbers From 176 To 222 Including Some Reynolds Number Effects
Download Longitudinal Aerodynamic Characteristics Of Two Blunted Cone Reentry Configurations At Mach Numbers From 176 To 222 Including Some Reynolds Number Effects full books in PDF, epub, and Kindle. Read online Longitudinal Aerodynamic Characteristics Of Two Blunted Cone Reentry Configurations At Mach Numbers From 176 To 222 Including Some Reynolds Number Effects ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
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:
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 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configuratons 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 Configuratons 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 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92 by :
Download or read book THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92 written by and published by . This book was released on 1961 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 by : James F. Campbell
Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Longitudinal Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half-cone at Mach Numbers to 0.92 by : George C. Kenyon
Download or read book The Longitudinal Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half-cone at Mach Numbers to 0.92 written by George C. Kenyon and published by . This book was released on 1961 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 by : Jim A. Penland
Download or read book Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 written by Jim A. Penland and published by . This book was released on 1961 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723195570 Total Pages :176 pages Book Rating :4.1/5 (955 download)
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 Administration (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 Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-18 with total page 176 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...
Book Synopsis Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8 by : P. Calvin Stainback
Download or read book Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8 written by P. Calvin Stainback and published by . This book was released on 1969 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4 by :
Download or read book Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4 written by and published by . This book was released on 1963 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by :
Download or read book 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 written by and published by . This book was released on 1959 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Reynolds Number and Model Support on the Supersonic Aerodynamic Chacteristics of a 140° Included-angle Cone by : Charles D. Trescot
Download or read book Effects of Reynolds Number and Model Support on the Supersonic Aerodynamic Chacteristics of a 140° Included-angle Cone written by Charles D. Trescot and published by . This book was released on 1974 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made in the Langley Unitary Plan wind tunnel to determine the effects of Reynolds number and sting-support interference on the static aerodynamic characteristics of a 140 deg-included-angle cone. Base pressures and forces and moments of the model were measured at Mach numbers of 1.50, 2.00, 2.94, and 4.00 for ratios of sting diameter to model diameter that varied from 0.125 to 0.500 through an angle-of-attack range from about minus 4 deg to 13 deg. The Reynolds number, based on model diameter 4.80 in. was varied from 161,000 to 415,000.
Book Synopsis Aerodynamic Characteristics at a Mach Number of 6.77 of a 9 ̊cone Configuration, with and Without Spherical Afterbodies, at Angles of Attack Up to 180 ̊with Various Degrees of Nose Blunting by : Luther Neal (Jr.)
Download or read book Aerodynamic Characteristics at a Mach Number of 6.77 of a 9 ̊cone Configuration, with and Without Spherical Afterbodies, at Angles of Attack Up to 180 ̊with Various Degrees of Nose Blunting written by Luther Neal (Jr.) and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of Short Blunt Cones with Various Nose and Base Cone Angles at Mach Numbers from 0.6 to 5.5 and Angles of Attack to 180 Degrees by : Stuart L. Treon
Download or read book Static Aerodynamic Characteristics of Short Blunt Cones with Various Nose and Base Cone Angles at Mach Numbers from 0.6 to 5.5 and Angles of Attack to 180 Degrees written by Stuart L. Treon and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing by : Edward J. Ray
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
