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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 Scientific and Technical Reports

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1966 with total page 1440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Selected Listing of NASA Scientific and Technical Reports for

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1965 with total page 1680 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 1969 with total page 1572 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Volume of Technical Papers Presented at AIAA Sounding Rocket Vehicle Technology Specialist Conference  Williamsburg  Virginia  February 28 March 1  1967

Download or read book A Volume of Technical Papers Presented at AIAA Sounding Rocket Vehicle Technology Specialist Conference Williamsburg Virginia February 28 March 1 1967 written by and published by . This book was released on 1967 with total page 610 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Collection of Technical Papers

Download or read book A Collection of Technical Papers written by and published by . This book was released on 1967 with total page 608 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA SP

    Book Details:
  • Author :
  • Publisher :
  • Release : 1962
  • ISBN :
  • Pages : 1426 pages

Download or read book NASA SP written by and published by . This book was released on 1962 with total page 1426 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Bibliography of Scientific and Industrial Reports

Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1965 with total page 964 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0   to 58   and Mach Numbers from 0 6 to 2 0

Download or read book Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 to 58 and Mach Numbers from 0 6 to 2 0 written by Leland Howard Jorgensen and published by . This book was released on 1974 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government wide Index to Federal Research   Development Reports

Download or read book Government wide Index to Federal Research Development Reports written by and published by . This book was released on 1965 with total page 1432 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Publications Announcements with Indexes

Download or read book Technical Publications Announcements with Indexes written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 1556 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Journal of the Royal Aeronautical Society

Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1964 with total page 1020 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0   to 58   and Mach Numbers from 0 6 to 2 0

Download or read book Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 to 58 and Mach Numbers from 0 6 to 2 0 written by Leland Howard Jorgensen and published by . This book was released on 1975 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Experimental Investigation at a Mach Number of 2 01 of the Effects of Body Cross section Shape on the Aerodynamic Characteristics of Bodies and Wing body Combinations

Download or read book An Experimental Investigation at a Mach Number of 2 01 of the Effects of Body Cross section Shape on the Aerodynamic Characteristics of Bodies and Wing body Combinations written by Harry W. Carlson and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: An experimental investigation has been performed to determine the effect of changes in body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations. A series of 13 bodies having a given length and given longitudinal distribution of cross-sectional area but various cross-section shapes were tested at a Mach number of 2.01. The bodies were tested alone and in combination with a 47° sweptback wing having a 6-percent-thick hexagonal section.

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.