Author: Abdollah Modavi
Publisher:
ISBN:
Category :
Languages : en
Pages : 286
Book Description
An Experimental Investigation of Supersonic Flow Past Circular Cones at High Angles of Attack
An Experimental Investigation of the Flow Field Around a Yawed Cone
Author: Robert H. Feldhuhn
Publisher:
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).
Publisher:
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).
Supersonic Aerodynamics of Large-angle Cones
Author: James F. Campbell
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 84
Book Description
Scientific and Technical Aerospace Reports
STAR
NASA Technical Note
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
A Selected Listing of NASA Scientific and Technical Reports for ...
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
Book Description
Missile Configuration Design
Author: S. S. Chin
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 304
Book Description
Beskriver principperne i f.m. konstruktionen af styrede missiler.
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 304
Book Description
Beskriver principperne i f.m. konstruktionen af styrede missiler.