Results 81 to 90 of about 81,739 (264)

Characteristic Performance of NAL 50cm Hypersonic Wind Tunnel

Journal of the Japan Society for Aeronautical and Space Sciences, 1971
The aerodynamic characteristics of the NAL 50cm hypersonic wind tunnel were tested at Mach numbers of 5, 7 and 9 with respect to Mach number and total temperature profiles at the test section, the effect of Reynolds numbes on the free stream Mach number, and boundary layer thickness at the nozzle exit, etc. Force tests of AGARD standard models HB-1 and
Itsu HIRAKI, Hideo NAGASU, Hiroshi HASHIZUME   +2 more
openaire   +2 more sources

Temporary Fiber Bragg Grating Sensors for Static and Dynamic Strain Measurements in Hypersonic Wind Tunnels

, 2023
Luke Pollock, Graham Wild
openalex   +2 more sources

87th Annual Meeting of the Meteoritical Society 2025: Abstracts

Meteoritics &Planetary Science, Volume 60, Issue S1, Page 30-350, August 2025.
wiley   +1 more source

Research on Shockwave/Boundary Layer Interactions Induced by Double Compression Corners Under Hypersonic Quiet and Noise Inflow Conditions

Aerospace
The problem of shock wave/boundary layer interaction induced by compression corners widely exists in the external and internal flows of various supersonic/hypersonic aircraft.
Dongsheng Zhang, Jinping Li, Hesen Yang, Hua Liang   +3 more
doaj   +1 more source

Measurements of freestream density fluctuations in a hypersonic wind tunnel

Experiments in Fluids, 2020
Byrenn Birch, D. Buttsworth, F. Zander
semanticscholar   +1 more source

A Review of Flow Control Strategies for Supersonic/Hypersonic Fluid Dynamics

Aerospace Research Communications
Supersonic and hypersonic flows have gained considerable attention in the aerospace industry in recent years. Flow control is crucial for refining the quality of these high-speed flows and improving the performance and safety of fast aircraft. This paper
Shibo Lee, Yunlong Zhao, Jiaqi Luo, Jianfeng Zou, Jifa Zhang, Jifa Zhang, Yao Zheng, Yao Zheng, Yang Zhang, Yang Zhang   +9 more
doaj   +1 more source

Renewed characterization of a Mach 6 hypersonic wind tunnel

, 2023
Sacha Hirsch, Guillaume Grossir, Olivier Chazot   +2 more
openalex   +2 more sources

Computational studies to determine the design of prototype heater for a hypersonic wind tunnel

, 2021
A S Rtishcheva
openalex   +1 more source

Ceramic and Coating Applications in the Hostile Environment of a High-Temperature Hypersonic Wind Tunnel [PDF]

, 2008
Richard L. Puster, J. R. Karns, Peter Vasquez, Warren C. Kelliher   +3 more
openalex   +1 more source

Effect of Distributed Roughness Elements on Crossflow Transition in a Yawed Cone in a Mach 6 Wind Tunnel

Aerospace
Research on hypersonic crossflow transition holds significant engineering and scientific importance. This paper investigates the impact of distributed roughness elements (DREs) on crossflow transition for a cone set at a 6° angle of attack, using ...
Haibo Niu, Shihe Yi, Xiaolin Liu, Jia Fu
doaj   +1 more source