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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

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:

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

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 Aerodynamic Performance and Static Stability Characteristics of a Blunt Nosed  Boattailed  13 Deg Half Cone at Mach Numbers from 0 6 to 5 0

Download or read book Aerodynamic Performance and Static Stability Characteristics of a Blunt Nosed Boattailed 13 Deg Half Cone at Mach Numbers from 0 6 to 5 0 written by and published by . This book was released on 1961 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Note

    Book Details:
  • Author :
  • Publisher :
  • Release : 1975
  • ISBN :
  • Pages : 616 pages

Download or read book NASA Technical Note written by and published by . This book was released on 1975 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics at Mach Numbers from 1 50 to 4 63 of a Variable geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control

Download or read book Aerodynamic Characteristics at Mach Numbers from 1 50 to 4 63 of a Variable geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control written by Roger H. Fournier and published by . This book was released on 1967 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.

Book Experimental Determination of Aerodynamic Drag on a Blunted 10 deg Cone at Angles of Attack in Hypersonic  Rarefied Flow

Download or read book Experimental Determination of Aerodynamic Drag on a Blunted 10 deg Cone at Angles of Attack in Hypersonic Rarefied Flow written by David E. Boylan and published by . This book was released on 1964 with total page 40 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 760 pages. Available in PDF, EPUB and Kindle. Book excerpt: