Author: Charles George MillerPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 90
Book Description
Langley Hotshot Tunnel Operations with Helium at Mach Numbers in Excess of 30
Author: Charles George MillerPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 90
Book Description
NASA Technical Note
Author: Applied Mechanics Reviews
Author: Scientific and Technical Aerospace Reports
Author: 30th AIAA Thermophysics Conference
Author: Program and Charts for Determining Shock Tube, Expansion Tube, and Expansion Tunnel Flow Quantities for Real Air
Author: Charles George MillerPublisher:
ISBN:
Category : Air flow
Languages : en
Pages : 284
Book Description
Operating Characteristics of the Langley Mach 10 High Reynolds Number Helium Tunnel
Author: Ralph D. WatsonPublisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 0
Book Description
The Aeronautical Journal
Author: A Survey of the Transport Properties of Helium at High Mach Number Wind-tunnel Conditions
Author: Dal V. MaddalonReal Gas Flow Parameters for NASA Langley 22-Inch Mach 20 Helium Tunnel
Author: Brian Ray HollisPublisher:
ISBN:
Category : Gases, Real
Languages : en
Pages :
Book Description