Design of axisymmetric contoured nozzles for laminar hypersonic flow.
- 1 September 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (9) , 1095-1100
- https://doi.org/10.2514/3.29427
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- HIGH TEMPERATURE, LOW DENSITY BOUNDARY-LAYER CONTROL BY CRYOGENIC PUMPINGPublished by Defense Technical Information Center (DTIC) ,1966
- Published by AIP Publishing ,1966
- Local heat-transfer coefficients in a nozzle with high-speed laminarflow.AIAA Journal, 1965
- SUPERSONIC AXISYMMETRIC NOZZLE DESIGN BY MASS FLOW TECHNIQUES UTILIZING A DIGITAL COMPUTERPublished by Defense Technical Information Center (DTIC) ,1964
- AERODYNAMIC DESIGN AND CALIBRATION OF THE VKF 50-INCH HYPERSONIC WIND TUNNELSPublished by Defense Technical Information Center (DTIC) ,1963
- A CALORIMETRIC INVESTIGATION OF SOME PROBLEMS ASSOCIATED WITH A LOW-DENSITY HYPERVELOCITY WIND TUNNELPublished by Defense Technical Information Center (DTIC) ,1963
- Heat Transfer to an Incompressible Turbulent Boundary Layer and Estimation of Heat-Transfer Coefficients at Supersonic Nozzle ThroatsJournal of the Aeronautical Sciences, 1956