Author:
Publisher:
ISBN: 9789283507529
Category : Guided missiles
Languages : en
Pages : 352
Book Description
Aérodynamique Des Missiles
Missile Aerodynamics (Aerodynamique Des Missiles).
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 507
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 507
Book Description
八火伝
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 360
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 360
Book Description
Special Course on Missile Aerodynamics
Author: Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial
Publisher:
ISBN: 9789283504528
Category : Guided missiles
Languages : en
Pages : 758
Book Description
Publisher:
ISBN: 9789283504528
Category : Guided missiles
Languages : en
Pages : 758
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 440
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 440
Book Description
Aerodynamic Data Accuracy and Quality
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 546
Book Description
The wind tunnel continues to be the main instrument for providing experimental aerodynamic data to the aerospace industry and the aerodynamic researcher for the purpose of load and performance evaluation and for verification of theoretical results. In both cases it is imperative that the user has confidence in the quality of the results, which means that he must have information on what accuracy to attach to the data. The quality of wind tunnel results depends upon both the accuracy of measurements and the imperfections provided by the wind tunnel environment. Great strides have been made in recent years on measurement accuracy and as a rule this need no longer be of much concern if properly attended to. However, imperfections provided by the wind tunnel environment are still with us and these are today the main sources affecting the quality and accuracy of aerodynamic data obtained in a wind tunnel. It was the purpose of this symposium to try to define what accuracy has presently been achieved in modern facilities and to compare these achievements with the actual demands of the user.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 546
Book Description
The wind tunnel continues to be the main instrument for providing experimental aerodynamic data to the aerospace industry and the aerodynamic researcher for the purpose of load and performance evaluation and for verification of theoretical results. In both cases it is imperative that the user has confidence in the quality of the results, which means that he must have information on what accuracy to attach to the data. The quality of wind tunnel results depends upon both the accuracy of measurements and the imperfections provided by the wind tunnel environment. Great strides have been made in recent years on measurement accuracy and as a rule this need no longer be of much concern if properly attended to. However, imperfections provided by the wind tunnel environment are still with us and these are today the main sources affecting the quality and accuracy of aerodynamic data obtained in a wind tunnel. It was the purpose of this symposium to try to define what accuracy has presently been achieved in modern facilities and to compare these achievements with the actual demands of the user.
Subsystem Integration for Tactical Missiles ( SITM ) and Design and Operation of Unmanned Air Vehicles ( DOUAV )
Author:
Publisher:
ISBN:
Category : Air warfare
Languages : en
Pages : 376
Book Description
Publisher:
ISBN:
Category : Air warfare
Languages : en
Pages : 376
Book Description
Effects of Magnus Moments on Missile Aerodynamic Performance
Author: George Y. Jumper (Jr.)
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 40
Book Description
Aerodynamic Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0
Author: J. H. Jones
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 220
Book Description
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the Beech High Altitude Supersonic Target (HAST) missile.
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 220
Book Description
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the Beech High Altitude Supersonic Target (HAST) missile.