Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Aerodynamic Characteristics At A Mach Number Of 677 Of A 9 Cone Configuration With And Without Spherical Afterbodies At Angles Of Attack Up To 180 With Various Degrees Of Nose Blunting
Download Aerodynamic Characteristics At A Mach Number Of 677 Of A 9 Cone Configuration With And Without Spherical Afterbodies At Angles Of Attack Up To 180 With Various Degrees Of Nose Blunting full books in PDF, epub, and Kindle. Read online Aerodynamic Characteristics At A Mach Number Of 677 Of A 9 Cone Configuration With And Without Spherical Afterbodies At Angles Of Attack Up To 180 With Various Degrees Of Nose Blunting ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
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 a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium by : Melvin J. Fohrman
Download or read book Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium written by Melvin J. Fohrman and published by . This book was released on 1963 with total page 48 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:
Book Synopsis Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 by : Lucille C. Coltrane
Download or read book Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 written by Lucille C. Coltrane and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° by : Leroy Devan
Download or read book Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° written by Leroy Devan and published by . This book was released on 1980 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares by : A. B. Carraway
Download or read book Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares written by A. B. Carraway and published by . This book was released on 1960 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp-and Blunt-nose Cones Having Flat and Modified Bases by : Sandia Corporation
Download or read book A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp-and Blunt-nose Cones Having Flat and Modified Bases written by Sandia Corporation and published by . This book was released on 1965 with total page 596 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 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-angle Cones with and Without Cylindrical Afterbodies by : James Franklin Campbell
Download or read book Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-angle Cones with and Without Cylindrical Afterbodies written by James Franklin Campbell and published by . This book was released on 1969 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and without cylindrical afterbodies.
Book Synopsis Aerodynamic Characteristics of a Modified Cone by : George C. Ashby
Download or read book Aerodynamic Characteristics of a Modified Cone written by George C. Ashby and published by . This book was released on 1968 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds by : K. R. Czarnecki
Download or read book Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds written by K. R. Czarnecki and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic High-angle-of-attack Aerodynamic Characteristics of a Cone and Cylinder with Triangular Cross Sections and a Cone with a Square Cross Section by :
Download or read book Subsonic High-angle-of-attack Aerodynamic Characteristics of a Cone and Cylinder with Triangular Cross Sections and a Cone with a Square Cross Section written by and published by . This book was released on 1983 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Spherically Blunted 25° Cone at a Mach Number of 20 by : Julius E. Harris
Download or read book Aerodynamic Characteristics of a Spherically Blunted 25° Cone at a Mach Number of 20 written by Julius E. Harris and published by . This book was released on 1967 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle by : Byron M. Jaquet
Download or read book Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle written by Byron M. Jaquet and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Aerodynamic Characteristics of 9 Deg Half-angle Cones with Varying Degrees of Bluntness at Mach Number 9 by : PHILCO NEWPORT BEACH CALIF AERONUTRONIC DIV.
Download or read book Experimental Investigation of the Aerodynamic Characteristics of 9 Deg Half-angle Cones with Varying Degrees of Bluntness at Mach Number 9 written by PHILCO NEWPORT BEACH CALIF AERONUTRONIC DIV. and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel test was conducted in a 21 in. hypersonic facility to obtain force and moment data on right circular cones of varying degrees of bluntness. Normal forces, axial forces, and pitching moments were measured over an angle of attack range of -10 to +15 degrees, at Mach numbers of 7.25 and 9.00, and a Reynolds number range of 0.037 to 0.150 x 10 to the 6th power/in. Three 9-degree half-angle cones with ratios of nose tip radius to base radius of 0.03, 0.187, and 0.30 were tested. The experimental data was compared with theoretical data, and the two were in good agreement. (Author).
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:
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...
