Wind tunnel simulation of multibooster separation trajectories of a launch vehicle
, 1995 Wind tunnel investigations were undertaken to study the separation characteristics of four strap-on boosters simultaneously separating from the core of a launch vehicle.
Lochan, R +4 more
core
Design and Experimental Study of an Over-Under TBCC Exhaust System. [PDF]
J Eng Gas Turbine Power, 2014 Mo J, Xu J, Zhang L.
europepmc +1 more source
Two dimentional transonic blockage interference studies in the NAL 1-Ft. blowdown wind tunnel
, 1974 Two 12% thick circular-arc aerof oils of 3 in. and 6 in. chord length were tested at zero angle of attack to determine the slot open-area ratio for minimum two-dimensional blockage interference at transonic speeds in the HAL 1-ft.
Ramaswamy, MA +2 more
core
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
, 1974 A series of slab wing flutter models with rigid orbiter fuselage, external tank, and SRB models of the space shuttle were tested, in a reflection plane arrangement, in the NASA Langley Research Center's 26-inch Transonic Blowdown Tunnel.
Kotch, M. A.
core
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.
europepmc +1 more source
, 2011 A supersonic wind tunnel, with a 20" x 20'" test section cross sectional area, was designed and constructed at the Techsburg Wind Tunnel Facility in order to determine the lift and drag on irregularly shaped fragments in supersonic flow.
Larson, Christopher Whitford
core
Flow characterization of the Mach 5 hypersonic nozzle of VKI-H3 wind tunnel
The operational map of the H3 Mach 6 blowdown wind tunnel, at the von Karman Institute for Fluid Dynamics (VKI), is extended towards lower Mach numbers with a new axisymmetric contoured nozzle to achieve Mach 5 testing conditions.
Chazot, Olivier +10 more
core +1 more source
Thermal pollution consequences of the implementation of the president's energy message on increased coal utilization. [PDF]
Environ Health Perspect, 1979 Parker FL.
europepmc +1 more source
Concept of variable mach number flexible nozzle and controls for NAL 0.6m blowdown wind tunnel
, 2009 In a supersonic wind tunnel, the contour of the nozzle, the second throat setting and the stagnation pressure controlled by the Pressure Regulating Valve (PRV) are fundamental parameters without which the required Mach number in the test section cannot ...
Basavaraju, NR +2 more
core