AERODYNAMIC TESTING AT MACH NUMBERS FROM 15 TO 20
- 1 January 1962
- book chapter
- Published by Elsevier
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Hypersonic Flow with Combined Leading-Edge Bluntness and Boundary-Layer Displacement EffectPublished by Defense Technical Information Center (DTIC) ,1960
- Theory of Stagnation Point Heat Transfer in Dissociated AirJournal of the Aerospace Sciences, 1958
- Shock-Wave Effects on the Laminar Skin Friction of an Insulated Flat Plate at Hypersonic SpeedsJournal of the Aeronautical Sciences, 1953