Author: Mamoru Inouye
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Wind-tunnel Measurements at Mach Numbers from 3 to 5 of Pressure and Turbulent Heat Transfer on a Blunt Cone-cylinder with Flared Afterbody
NASA Technical Note
Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1746
Book Description
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1746
Book Description
Scientific and Technical Aerospace Reports
A Description of Numerical Methods and Computer Programs for Two-dimensional and Axisymmetric Supersonic Flow Over Blunt-nosed and Flared Bodies
Author: Mamoru Inouye
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 42
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
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1680
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1680
Book Description
Index Aeronauticus
Effects of Mach Number and Wall-temperature Ratio on Turbulent Heat Transfer at Mach Numbers from 3 to 5
Author: Thorval Tendeland
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 24
Book Description