Author: Abdollah ModaviPublisher:
ISBN:
Category :
Languages : en
Pages : 286
Book Description
An Experimental Investigation of Supersonic Flow Past Circular Cones at High Angles of Attack
Author: Abdollah ModaviAn Experimental Investigation of the Flow Field Around a Yawed Cone
Author: Robert H. FeldhuhnPublisher:
ISBN:
Category : Cone
Languages : en
Pages : 106
Book Description
An experimental investigation of the flow field associated with a highly yawed cone was conducted at a Mach number of 5 and a free-stream Reynolds number per foot of 4,400,000. Surface static pressure measurements, flow-field surveys and schlieren photographs were obtained on a sharp five-degree semi-vertex angle cone at an angle of attack of 24 degrees. The results of the measurements indicate that the flow field on the leeward side of a highly yawed cone is very similar to that of a circular cylinder in supersonic cross flow. The essential difference between these two flow fields is the presence of a disturbance from the tip of the cone which separates the gas which has passed through the shock wave on the windward side from the flow which has passed through the weaker portion of the shock wave on the leeward side of the cone. (Author).
An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack
Author: Robert H. FeldhuhnPublisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 148
Book Description
Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.
Scientific and Technical Aerospace Reports
Author: WADC Technical Report
Author: United States. Wright Air Development DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1276
Book Description
Experimental Investigation of the Effect of Vertical-tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 ̊sweptback Wing and Tail Surfaces
Author: Antonio FerriPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 328
Book Description
Investigation of the Normal-force, Axial-force, and Pitching-moment Characteristics of Blunt Low-fineness-ratio Bodies of Revolution at a Mach Number of 3.55
Author: Russell W. McDearmonPublisher:
ISBN:
Category : Axial loads
Languages : en
Pages : 38
Book Description
NASA Technical Report
Author: An Experimental Investigation of the Turbulent Boundary Layer in Supersonic Flow Around Unyawed Cones with Small Heat Transfer and Correlations with Two Dimensional Data
Author: Walter Samuel BradfieldPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 344
Book Description
Author: