Cavitation Inception - A Selective Review [PDF]
, 1975 This paper reviews recent developments in selected cavitation research areas which have been active mainly within the past two years. The new understanding resulting from this work is summarized.
Acosta, A. J., Parkin, B. R.
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Decomposition of nitric oxide in a hot nitrogen stream to synthesize air for hypersonic wind tunnel combustion testing [PDF]
A clean source of high enthalpy air was obtained from the exothermic decomposition of nitric oxide in the presence of strongly heated nitrogen. A nitric oxide jet was introduced into a confined coaxial nitrogen stream.
Zlatarich, S. A., Zumdieck, J. F.
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Exploratory studies of the cruise performance of upper surface blown configurations. Experimental program: Test facilities, model design instrumentation, and lowspeed, high-lift tests [PDF]
The model hardware, test facilities and instrumentation utilized in an experimental study of upper surface blown configurations at cruise is described.
Braden, J. A. +3 more
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Historical perspectives on thermostructural research at the NACA Langley Aeronautical Laboratory from 1948 to 1958 [PDF]
Some of the early research on structural problems produced by aerodynamic heating, conducted at the Langley Aeronautical Laboratory of the National Advisory Committee for Aeronautics from 1948 to 1958 is described.
Heldenfels, R. R.
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Experimental studies of hypersonic boundary-layer transition and effects of wind tunnel disturbances [PDF]
Boundary layer transition data on cones and free stream disturbance levels were measured in a hypersonic wind tunnel and Mach 8 variable density hypersonic tunnel.
Horstman, C. C. +3 more
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Analytical and experimental study of the effects of wing-body aerodynamic interaction on space shuttle subsonic flutter [PDF]
The effects on flutter of the aerodynamic interaction between the space shuttle bodies and wing, 1/80th-scale semispan models of the orbiter wing, the complete shuttle and intermediate component combinations were tested in the NASA Langley Research ...
Chipman, R. R., Rauch, F. J.
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Design and Experimental Study of an Over-Under TBCC Exhaust System. [PDF]
J Eng Gas Turbine Power, 2014 Mo J, Xu J, Zhang L.
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Correction of four-percent Saturn 5 model protuberance test data [PDF]
Data reduction of transonic wind tunnel static pressure variation tests for correcting Saturn 5 ...
Mc Canless, G. F., Jr.
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Numerical study on the start and unstart phenomena in a scramjet inlet-isolator model. [PDF]
PLoS One, 2019 Lee J, Kang SH.
europepmc +1 more source
Penetration Characteristics of Air, Carbon Dioxide and Helium Transverse Sonic Jets in Mach 5 Cross Flow. [PDF]
Sensors (Basel), 2014 Erdem E, Kontis K, Saravanan S.
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