Author: Owen H. Davis
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
Performance of a Mach Number 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range 1.97 to 0.79
Author: Owen H. Davis
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8
Author: John L. Allen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24
Book Description
Performance of a Mach 3.0 External-internal- Compression Axisymmetric Inlet at Mach Numbers from 2.0 to 3.5
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
Effect of External Boundary Layer on Performance of Axisymmetric Inlet at Mach Numbers of 3.0 and 2.5
Author: N. E. Samanich
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
Book Description
Performance of Three Isentropic All Internal Compression Axisymmetric Inlets Designed for Mach 2.5
Author: Bernhard H. Anderson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 34
Book Description
A Comparison of the Performance of Four Side-mounted Inlets Over a Mach Number Range of 0.88 to 2.2 and Angles of Attack to 14°
Author: Leroy L. Presley
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 58
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 58
Book Description
Investigation of Three Mach 7 External Compression Axisymmetric Inlets from Mach 1.9 to 6.8
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Investigation of an Axisymmetric Internal Compression Inlet at a Mach Number of about 3.8
Author: John H. Lundell
Publisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 38
Book Description
Performance of an Axisymmetric External-compression and a Two-dimensional External-internal-compression Inlet at Mach 4.95
Author: James F. Connors
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
Book Description
PERFORMANCE SUMMARY AND ANALYSIS OF A MACH 3.0 DESIGN AXISYMMETRIC ALL-EXTERNAL-COMPRESSION DOUBLE-CONE INLET FROM MACH NUMBER 3.0 TO 0.8
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description