EDP Sciences logo
Submit your paper
Search
Menu
All issues Volume 43 / No 5 (October 2025) JNWPU, 43 5 (2025) 862-868 References
Open Access
Issue
JNWPU
Volume 43, Number 5, October 2025
Page(s) 862 - 868
DOI https://doi.org/10.1051/jnwpu/20254350862
Published online 05 December 2025
  1. VARNER M O, SUMMERS W E, DAVIS M W. A review of two-dimensional nozzle design techniques[R]. AIAA-1982-0609, 1982 [Google Scholar]
  2. MEYER R E, HOLT M. The correction of wind tunnel nozzles for two-dimensional supersonic flow[J]. The Aeronautical Quarterly, 1950, 2: 195 [Article] [Google Scholar]
  3. MAC D. Correction of flexible plate supersonic nozzle contours by influence method[J]. Journal of the Aeronautical Sciences, 1955, 22(5): 289–296 [Article] [Google Scholar]
  4. XU Huafang. Fundamentals of aerodynamics[M]. Beijing: National Defense Industry Press, 1987 (in Chinese) [Google Scholar]
  5. PRANDTL L, BUSEMANN A. Naherungsverfahren ZUR zeichnerischen ermittlung von ebenen stromungen mit uberschallgeschwindigkeit[C]//Stodola Festschrift, 1929: 499–509 [Google Scholar]
  6. PUCKETT A E. Supersonic nozzle design[J]. Journal of Applied Mechanics, 1946, 13(4): 265–270 [Article] [Google Scholar]
  7. FOELSCH K. A new method of designing two-dimensional laval nozzles for a parallel and uniform jet[R]. NA-46-235-1, 1946 [Google Scholar]
  8. FOELSCH K. The analytical design of an axially symmetric laval nozzle for a parallel and uniform jet[J]. Journal of the Aeronautical Sciences, 1949, 16(188): 161–166 [Google Scholar]
  9. CROWN J C. Supersonic nozzle design[R]. NACA TN 1651, 1948 [Google Scholar]
  10. SIVELLS J C. Analytic determination of two-dimensional supersonic nozzle contours having continuous curvature[R]. AEDC-TR-1956-11, 1956 [Google Scholar]
  11. SIVELLS J C, PAYNE R G. A method of calculating turbulent-boundary-layer growth at hypersonic mach numbers[R]. AEDC-TR-1959-3, 1959 [Google Scholar]
  12. LIAO Daxiong, CHEN Jiming, PENG Qiang, et al. Key design techniques of continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(4): 74–78 (in Chinese) [Google Scholar]
  13. LIAO Daxiong, CHEN Jiming, ZHENG Juan, et al. General performance of 0.6 m continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(6): 88–93 (in Chinese) [Google Scholar]
  14. CHEN Jiming, WU Shenghao, LIAO Daxiong, et al. Experimental study for improving flow-field quality for 0.6 m continuous transonic wind tunnel[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2021, 53(2): 236–242 (in Chinese) [Google Scholar]
  15. CHEN Zhenhua, LIU Zongzheng, CHEN Jiming, et al. Characteristics and key technology analysis of large continuous transonic wind tunel[J]. Journal of Experiments in Fluid Mechanics, 2022, 36(1): 62–68 (in Chinese) [Google Scholar]
  16. GJB 1179A—2012, 2012 General Armaments Department of the People's Liberation Army. Requirement for flow quality of low and high speed wind tunnels[S]. GJB 1179A—2012, 2012 (in Chinese) [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.