Author: Kenneth K. Kuo
Publisher: Taylor & Francis
ISBN: 9780891169376
Category : Science
Languages : en
Pages : 336
Book Description
Includes papers presented at a symposium, which represent the state-of-the-art in the development of base bleed projectiles and related research, and are from recognized experts in the field. The papers have undergone a thorough review process.
Base Bleed
Author: Kenneth K. Kuo
Publisher: Taylor & Francis
ISBN: 9780891169376
Category : Science
Languages : en
Pages : 336
Book Description
Includes papers presented at a symposium, which represent the state-of-the-art in the development of base bleed projectiles and related research, and are from recognized experts in the field. The papers have undergone a thorough review process.
Publisher: Taylor & Francis
ISBN: 9780891169376
Category : Science
Languages : en
Pages : 336
Book Description
Includes papers presented at a symposium, which represent the state-of-the-art in the development of base bleed projectiles and related research, and are from recognized experts in the field. The papers have undergone a thorough review process.
NASA Technical Report
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 52
Book Description
Flow in the Base Region of Axisymmetric and Two-dimensional Configurations
Author: Milton A. Beheim
Publisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 44
Book Description
A theoretical and experimental investigation has been conducted of the pressure distribution on the surface of either a circular cylinder or a truncated cone located within the base region of another circular cylinder at Mach number 2. A similar analysis of pressure distribution was made for rearward-facing two-dimensional steps, and theoretical results were compared with experimental results of earlier investigations. Theoretical base-pressure ratios of two-dimensional steps agreed well with experimental results; however, as a result of the simplifying assumptions made for axisymmetric configurations, only a range of values for theoretical base-pressure ratio could be calculated within which the experimental results were expected to occur. The data generally followed the trends predicted by the theory, and deviations apparently could be explained.
Publisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 44
Book Description
A theoretical and experimental investigation has been conducted of the pressure distribution on the surface of either a circular cylinder or a truncated cone located within the base region of another circular cylinder at Mach number 2. A similar analysis of pressure distribution was made for rearward-facing two-dimensional steps, and theoretical results were compared with experimental results of earlier investigations. Theoretical base-pressure ratios of two-dimensional steps agreed well with experimental results; however, as a result of the simplifying assumptions made for axisymmetric configurations, only a range of values for theoretical base-pressure ratio could be calculated within which the experimental results were expected to occur. The data generally followed the trends predicted by the theory, and deviations apparently could be explained.
Research in Progress
Author:
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 652
Book Description
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 652
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 104
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 104
Book Description
40th AIAA Aerospace Sciences Meeting & Exhibit
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 710
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 710
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Jet effects on annular base pressure and temperature in a supersonic stream
Author: Milton A. Beheim
Publisher:
ISBN:
Category : Gases at high temperatures
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Gases at high temperatures
Languages : en
Pages : 52
Book Description
AIAA Journal
Author: American Institute of Aeronautics and Astronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1184
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1184
Book Description
Analytical Study of Soft Landings on Gas-filled Bags
Author: Jack B. Esgar
Publisher:
ISBN:
Category : Gas
Languages : en
Pages : 732
Book Description
Publisher:
ISBN:
Category : Gas
Languages : en
Pages : 732
Book Description