Experimental studies of a laminar hypersonic cone wake.
- 1 September 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (9) , 1724-1730
- https://doi.org/10.2514/3.5382
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Experimental studies of a laminar hypersonic cone wake.AIAA Journal, 1969
- Experimental Investigation of Laminar Near Wakes Behind 20 Wedges M=6AIAA Journal, 1968
- A new theoretical solution of the laminar, hypersonic near wakePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Further results of viscous interaction theory for the laminar supersonic near wakePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Near wake uniqueness and a re-examination of the throat concept in laminar mixing theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- A study of laminar near wakes.AIAA Journal, 1966
- An experimental investigation of the near wake of a slender cone at M infinity equal 8 and 12.AIAA Journal, 1966
- Magnetic Suspension with Minimum Coupling Effects for Wind Tunnel ModelsIEEE Transactions on Aerospace and Electronic Systems, 1965
- Hypersonic wakes and trailsAIAA Journal, 1964
- An Experimental Investigation of Base Flows at Supersonic SpeedsJournal of the Royal Aeronautical Society, 1961