Fluctuating pressures due to shock interactions with turbulence and sound - interaction of escape tower wake turbulence with separation shoc
The results of sonic boom research studies are presented. The purpose of the studies was as follows:...
Thesis. 1977. Ph.D. cn--Massachusetts Institute of Technology. Dept. of PhysicsVita.Includes bibliog...
Relation of Eulerian and Lagrangian structure of pseudosound pressure and velocity fields in turbule...
Aerodynamic noise research - acoustic environment due to separated flows and oscillating shocks and ...
Fluctuating surface pressures due to shock wave interactions with turbulence and sound wave
Turbulent flow field around supersonic space vehicles - identification of separated flow component
Pressure fluctuations caused by turbulence interaction with shock and expansion wave
Issued as Quarterly status report [1-5], and Final report, Project no. E-16-611 (formerly B-221)Fina...
Experimental data were obtained on blade self-noise generation by strong adverse-pressure-gradient a...
Probe separates sound waves from turbulent flow pressure fluctuations in ducted airstreams by using ...
October 1970Includes bibliographical references (leaf 10)The noise produced by convection of turbule...
The results of this thesis demonstrate that direct numerical simulation can predict sound generation...
Shock-panel coupling effects of supersonic turbulent flow driven by impedance hea
A facility that was used to measure the interaction of flow with sound at high Mach numbers is descr...
Many supersonic military aircraft and some of the modern civilian aircraft (such as the Boeing 777) ...
The results of sonic boom research studies are presented. The purpose of the studies was as follows:...
Thesis. 1977. Ph.D. cn--Massachusetts Institute of Technology. Dept. of PhysicsVita.Includes bibliog...
Relation of Eulerian and Lagrangian structure of pseudosound pressure and velocity fields in turbule...
Aerodynamic noise research - acoustic environment due to separated flows and oscillating shocks and ...
Fluctuating surface pressures due to shock wave interactions with turbulence and sound wave
Turbulent flow field around supersonic space vehicles - identification of separated flow component
Pressure fluctuations caused by turbulence interaction with shock and expansion wave
Issued as Quarterly status report [1-5], and Final report, Project no. E-16-611 (formerly B-221)Fina...
Experimental data were obtained on blade self-noise generation by strong adverse-pressure-gradient a...
Probe separates sound waves from turbulent flow pressure fluctuations in ducted airstreams by using ...
October 1970Includes bibliographical references (leaf 10)The noise produced by convection of turbule...
The results of this thesis demonstrate that direct numerical simulation can predict sound generation...
Shock-panel coupling effects of supersonic turbulent flow driven by impedance hea
A facility that was used to measure the interaction of flow with sound at high Mach numbers is descr...
Many supersonic military aircraft and some of the modern civilian aircraft (such as the Boeing 777) ...
The results of sonic boom research studies are presented. The purpose of the studies was as follows:...
Thesis. 1977. Ph.D. cn--Massachusetts Institute of Technology. Dept. of PhysicsVita.Includes bibliog...
Relation of Eulerian and Lagrangian structure of pseudosound pressure and velocity fields in turbule...
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