Rao, DM and Murthy, AV and Kashyap, RR (1976) A variable by-pass diffuser for supersonic wind tunnels. Journal of Aeronautical Society of India, 28 . pp. 27-31.Full text not available from this repository.
The feasibility of a by-pass variable diffuser of simple concept for supersonic wind tunnels has been investigated experimentally at Mach numbers 2.5 and 3.0. With this design, minimum running stagnation pressures comparable to that obtainable with a conventional type variable diffuser were achieved. Present results indicated possibilities of further aerodynamic improvement for which simple modifications have been suggested.
|Item Type:||Journal Article|
|Uncontrolled Keywords:||Diffusers;Wind tunnels;Supersonic aircraft;Aeronautics; Modification;Stagnation;Aerodynamics; Realizability; Aerodynamic characteristics;Supersonic wind tunnels;Wind tunnels;Wind tunnel apparatus;Mach number;Stagnation pressure13;|
|Subjects:||AERONAUTICS > Aerodynamics|
|Division/Department:||Aerodynamics, Aerodynamics, Aerodynamics|
|Depositing User:||M/S ICAST NAL|
|Date Deposited:||05 Jan 2007|
|Last Modified:||24 May 2010 09:54|
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