Author: David E. Boylan
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 68
Book Description
The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9 and +10 deg in a low-density, hypersonic wind tunnel. Circumferential and longitudinal distributions are presented for cold wall conditions for a range at Mach and Reynolds numbers. The effect of source-like flows was studied by utilizing both conical and contoured expansion nozzles with the same free-stream similarity parameters and model wall temperatures. Comparisons are made with previously published experimental and theoretical results. (Author).
Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow
Author: David E. Boylan
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 68
Book Description
The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9 and +10 deg in a low-density, hypersonic wind tunnel. Circumferential and longitudinal distributions are presented for cold wall conditions for a range at Mach and Reynolds numbers. The effect of source-like flows was studied by utilizing both conical and contoured expansion nozzles with the same free-stream similarity parameters and model wall temperatures. Comparisons are made with previously published experimental and theoretical results. (Author).
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 68
Book Description
The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9 and +10 deg in a low-density, hypersonic wind tunnel. Circumferential and longitudinal distributions are presented for cold wall conditions for a range at Mach and Reynolds numbers. The effect of source-like flows was studied by utilizing both conical and contoured expansion nozzles with the same free-stream similarity parameters and model wall temperatures. Comparisons are made with previously published experimental and theoretical results. (Author).
Scientific and Technical Aerospace Reports
Static Pressure on Sharp and Blunt Cones in Conical and Parallel Low-density Flow
Author: Max Kinslow
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 78
Book Description
The static pressure distribution on sharp and blunt 10-deg half-angle cones was measured under rarefied conditions in both a uniform and a source flow field. Angle of attack of the cones was varied up to 10 deg. Pressure distributions are presented for cold-wall conditions at 18.0 = or
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 78
Book Description
The static pressure distribution on sharp and blunt 10-deg half-angle cones was measured under rarefied conditions in both a uniform and a source flow field. Angle of attack of the cones was varied up to 10 deg. Pressure distributions are presented for cold-wall conditions at 18.0 = or
Laminar Heat-transfer Distributions on Biconics at Incidence in Hypersonic-hypervelocity Flows
Author: Charles G. Miller (III.)
Publisher:
ISBN:
Category :
Languages : en
Pages : 178
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 178
Book Description
Laminar Heat-transfer Distributions on Biconics at Incidence in Hypersonic-hypervelocity Flows
Author: Charles George Miller
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 152
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 152
Book Description
Numerical Methods in Laminar and Turbulent Flow
Author: Cedric Taylor
Publisher:
ISBN:
Category : Mathematics
Languages : en
Pages : 1032
Book Description
Publisher:
ISBN:
Category : Mathematics
Languages : en
Pages : 1032
Book Description
Government Reports Index
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 908
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 908
Book Description
Outer Planet Entry Heating and Thermal Protection
Author: Raymond Viskanta
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 432
Book Description
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 432
Book Description