Hypersonic viscous drag effects on blunt slender cones
- 1 October 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (10) , 1714-1722
- https://doi.org/10.2514/3.2658
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Laminar heat transfer to spherically blunted cones at hypersonic conditionsAIAA Journal, 1964
- Status of Development of Hotshot Tunnels at the AedcPublished by Elsevier ,1964
- VISCOUS EFFECTS ON ZERO-LIFT DRAG OF SLENDER BLUNT CONESPublished by Defense Technical Information Center (DTIC) ,1963
- HYPERSONIC FLOW OVER A SLENDER CONE WITH GAS INJECTIONPublished by Defense Technical Information Center (DTIC) ,1962
- AERODYNAMIC TESTING AT MACH NUMBERS FROM 15 TO 20Published by Elsevier ,1962
- DESCRIPTION AND PRELIMINARY CALIBRATION OF A LOW-DENSITY, HYPERVELOCITY WIND TUNNELPublished by Defense Technical Information Center (DTIC) ,1961
- The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1956