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Book A Parametric Study of the Aerodynamic Characteristics of Nose cylinder flare Bodies at a Mach Number of 6 0

Download or read book A Parametric Study of the Aerodynamic Characteristics of Nose cylinder flare Bodies at a Mach Number of 6 0 written by George C. Ashby and published by . This book was released on 1965 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Note

    Book Details:
  • Author :
  • Publisher :
  • Release : 1965
  • ISBN :
  • Pages : 404 pages

Download or read book NASA Technical Note written by and published by . This book was released on 1965 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Investigation to Determine the Stability Characteristics of Three Supersonic impact Ballistic Reentry Shapes at Mach Numbers from 1 2 to 4 2

Download or read book An Investigation to Determine the Stability Characteristics of Three Supersonic impact Ballistic Reentry Shapes at Mach Numbers from 1 2 to 4 2 written by and published by . This book was released on 1962 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 912 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics in Pitch of Several Triple body Missile Configurations at Mach Numbers 0 6 to 1 4

Download or read book Aerodynamic Characteristics in Pitch of Several Triple body Missile Configurations at Mach Numbers 0 6 to 1 4 written by Earl D. Knechtel and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1978 with total page 996 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Book Aerodynamic Characteristics in Pitch of a Series of Cruciform wing Missiles with Canard Controls at a Mach Number of 2 01

Download or read book Aerodynamic Characteristics in Pitch of a Series of Cruciform wing Missiles with Canard Controls at a Mach Number of 2 01 written by M. Leroy Spearman and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1 10 scale Model of the Blue Scout Jr  at Mach Numbers from 0 40 to 1 03

Download or read book Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1 10 scale Model of the Blue Scout Jr at Mach Numbers from 0 40 to 1 03 written by Thomas C. Kelly and published by . This book was released on 1962 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics of a Group of Winged Reentry Vehicles at Mach Number 6 01 at Angles of Attack from 60 to 120 and  10 to 30 Roll at 90 Angle of Attack

Download or read book Aerodynamic Characteristics of a Group of Winged Reentry Vehicles at Mach Number 6 01 at Angles of Attack from 60 to 120 and 10 to 30 Roll at 90 Angle of Attack written by James G. Hondros and published by . This book was released on 1961 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book 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

Download or read book 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 written by Ross B. Robinson and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics at Mach Numbers from 1 60 to 2 16 of a Blunt nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins

Download or read book Aerodynamic Characteristics at Mach Numbers from 1 60 to 2 16 of a Blunt nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins written by William J. Monta and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics of a Group of Winged Reentry Vehicles at Mach Number 6 01 at Angles of Attack from 60 Deg to 120 Deg and Minus 10 Deg to 30 Deg Roll at 90 Deg Angle of Attack

Download or read book Aerodynamic Characteristics of a Group of Winged Reentry Vehicles at Mach Number 6 01 at Angles of Attack from 60 Deg to 120 Deg and Minus 10 Deg to 30 Deg Roll at 90 Deg Angle of Attack written by and published by . This book was released on 1961 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics in Pitch and Sideslip of a 1 15 scale Model of the Scout Vehicle at a Mach Number of 2 01

Download or read book Aerodynamic Characteristics in Pitch and Sideslip of a 1 15 scale Model of the Scout Vehicle at a Mach Number of 2 01 written by Ross B. Robinson and published by . This book was released on 1961 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book U S  Government Research Reports

Download or read book U S Government Research Reports written by and published by . This book was released on 1962-07 with total page 418 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Recent Advances in Aerospace Engineering

Download or read book Recent Advances in Aerospace Engineering written by Sanjay Singh and published by Springer Nature. This book was released on with total page 605 pages. Available in PDF, EPUB and Kindle. Book excerpt: