Nothing Special   »   [go: up one dir, main page]

Gildfind et al., 2015 - Google Patents

Performance considerations for expansion tube operation with a shock-heated secondary driver

Gildfind et al., 2015

View PDF
Document ID
7132709142645544332
Author
Gildfind D
James C
Toniato P
Morgan R
Publication year
Publication venue
Journal of Fluid Mechanics

External Links

Snippet

A shock-heated secondary driver is a modification typically applied to an expansion tube which involves placing a volume of helium between the primary diaphragm and the test gas. This modification is normally used to either increase the driven shock strength through the …
Continue reading at core.ac.uk (PDF) (other versions)

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02Wind tunnels

Similar Documents

Publication Publication Date Title
Gildfind et al. Performance considerations for expansion tube operation with a shock-heated secondary driver
Gildfind et al. Expansion tubes in Australia
Collen et al. Development and commissioning of the T6 Stalker Tunnel
Gardner et al. Ground testing of the HyShot supersonic combustion flight experiment in HEG and comparison with flight data
Sasoh et al. Supersonic drag reduction with repetitive laser pulses through a blunt body
Holden et al. Experimental studies in the LENS supersonic and hypersonic tunnels for hypervelocity vehicle performance and code validation
Mundt et al. Validation study of numerical simulations by comparison to measurements in piston-driven shock-tunnels
Bashor et al. Design and Preliminary Calibration of the UTSA Mach 7 Hypersonic Ludwieg Tube
Chue et al. Studies of the transient flows in high enthalpy shock tunnels
Stennett et al. Performance optimization of X3R: A new reflected shock tunnel mode for the X3 expansion tube
Cooper et al. The effect of transient nozzle flow on detonation tube impulse
Chinske et al. Visualization and Measurement of Transverse Jet Injection on a 7 Degree Half-Angle Cone in Hypersonic Quiet Flow
Borovoi et al. Two-dimensional interaction between an incident shock and a turbulent boundary layer in the presence of an entropy layer
James et al. Experimentally simulating gas giant entry in an expansion tube
Abul-Huda et al. Design and characterization of the Michigan hypersonic expansion tube facility (MHExT)
Subiah et al. Condition development and commissioning of the Oxford T6 Stalker Tunnel in reflected shock tunnel mode
Chang Design and development of a rectangular supersonic wind tunnel facility for the study of shock/boundary layer interactions
James et al. On the current limits of simulating gas giant entry flows in an expansion tube
Andrianatos et al. Preliminary development of high enthalpy conditions for the X3 expansion tube
Steer et al. LASTA 2.0: Validation of a Reverse Time Integration Method
Stennett et al. Large-scale free-piston-driven multi-mode shock expansion tunnel
Morgan et al. Impulse facility simulation of hypervelocity radiating flows
Toniato et al. Development of a new Mach 12 scramjet operating capability in the X3 expansion tube
Chung et al. Adiabatic-compression preheated Ludwieg tube for the realistic simulation of hypersonic flows
Gildfind et al. Simulation of high mach number scramjet flow conditions using the X2 expansion tube