Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725986978
Category :
Languages : en
Pages : 38
Book Description
Heat transfer rates and pressures were obtained on an elevon plate (deflected 30 deg) and a flat plate upstream of the elevon in an 8 foot high-temperature structures tunnel. The flight Reynolds number and flight total enthalpy for altitudes of 26.8 km and 28.7 km at Mach seven were duplicated. The heat transfer and pressure data were used to establish heating and pressure loads. The measured heating was compared with several theoretical predictions, and the closest agreement obtained with a Schultz-Grunow reference enthalpy method of calculation. Johnson, C. B. and Taylor, A. H. and Weinstein, I. Langley Research Center NASA-TM-X-3563, L-11524 RTOP 505-11-31-02...
Heat-Transfer and Pressure Measurements on a Simulated Elevon Deflected 30 Deg Near Flight Conditions at Mach 7
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725986978
Category :
Languages : en
Pages : 38
Book Description
Heat transfer rates and pressures were obtained on an elevon plate (deflected 30 deg) and a flat plate upstream of the elevon in an 8 foot high-temperature structures tunnel. The flight Reynolds number and flight total enthalpy for altitudes of 26.8 km and 28.7 km at Mach seven were duplicated. The heat transfer and pressure data were used to establish heating and pressure loads. The measured heating was compared with several theoretical predictions, and the closest agreement obtained with a Schultz-Grunow reference enthalpy method of calculation. Johnson, C. B. and Taylor, A. H. and Weinstein, I. Langley Research Center NASA-TM-X-3563, L-11524 RTOP 505-11-31-02...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725986978
Category :
Languages : en
Pages : 38
Book Description
Heat transfer rates and pressures were obtained on an elevon plate (deflected 30 deg) and a flat plate upstream of the elevon in an 8 foot high-temperature structures tunnel. The flight Reynolds number and flight total enthalpy for altitudes of 26.8 km and 28.7 km at Mach seven were duplicated. The heat transfer and pressure data were used to establish heating and pressure loads. The measured heating was compared with several theoretical predictions, and the closest agreement obtained with a Schultz-Grunow reference enthalpy method of calculation. Johnson, C. B. and Taylor, A. H. and Weinstein, I. Langley Research Center NASA-TM-X-3563, L-11524 RTOP 505-11-31-02...
Heat-transfer and Pressure Measurements on a Simulated Elevon Deflected 30 Deg Near Flight Conditions at Mach 7
Author: C. B. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Heat-transfer and Pressure Measurements on a Simulated Elevon Deflected 30 ̊near Flight Conditions at Mach 7
Author: Charles B. Johnson
Publisher:
ISBN:
Category : Aeronautics, Hypersonic
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aeronautics, Hypersonic
Languages : en
Pages : 40
Book Description
Heat-transfer and Pressure Measurements on a Simulated Elevon Deflected 30° Near Flight Conditions at Mach 7
Author: Charles B. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Heat-transfer and Pressure Measurements on a Simulated Elevon Deflected 30 N̊ear Flight Conditions at Mach 7
Author: Charles B. Johnson
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 34
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 548
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 548
Book Description
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
Evaluation of Three Thermal Protection Systems in a Hypersonic High-heating-rate Environment Induced by an Elevon Deflected 30 Deg
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 152
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 152
Book Description
R & D Abstracts
Author: Technology Reports Centre (Great Britain)
Publisher:
ISBN:
Category :
Languages : en
Pages : 460
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 460
Book Description