Author: Joseph W. Cleary
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 82
Book Description
An Experimental and Theoretical Investigation of the Pressure Distribution and Flow Fields of Blunted Cones at Hypersonic Mach Number
Author: Joseph W. Cleary
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 82
Book Description
An Experimental and Theoretical Investigation of the Pressure Distribution and Flow Fields of Blunted Cones at Hypersonic Mach Numbers
NASA Technical Note
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).
Advances in Aeronautical Sciences
Author: Th. Von Kármán
Publisher: Elsevier
ISBN: 1483223361
Category : Technology & Engineering
Languages : en
Pages : 591
Book Description
Advances in Aeronautical Sciences, Volume 2 contains the proceedings of the First International Congress in the Aeronautical Sciences, held in Madrid, Spain in September 1958. The book is comprised of survey papers and original contributions that discuss common problems in aeronautics and in space technology. The text presents interesting articles that deals with topics on the fundamental design problems of aircraft with boundary layer control for maintaining laminar flow; developments in hypersonic flow research; structures and materials for finite lifetime; and propulsion methods in astronautics. Aeronautics engineers and scientists in allied fields will find the book invaluable.
Publisher: Elsevier
ISBN: 1483223361
Category : Technology & Engineering
Languages : en
Pages : 591
Book Description
Advances in Aeronautical Sciences, Volume 2 contains the proceedings of the First International Congress in the Aeronautical Sciences, held in Madrid, Spain in September 1958. The book is comprised of survey papers and original contributions that discuss common problems in aeronautics and in space technology. The text presents interesting articles that deals with topics on the fundamental design problems of aircraft with boundary layer control for maintaining laminar flow; developments in hypersonic flow research; structures and materials for finite lifetime; and propulsion methods in astronautics. Aeronautics engineers and scientists in allied fields will find the book invaluable.
Government-wide Index to Federal Research & Development Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 980
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 980
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
Book Description