Shaping of airplane fuselages for minimum drag
- 1 May 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 24 (5) , 298-304
- https://doi.org/10.2514/3.45444
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Manufacturing Tolerances for Natural Laminar Flow Airframe SurfacesSAE International Journal of Advances and Current Practices in Mobility, 1985
- Assessing the Effect of Stylus Tip Radius and Flight on Surface Topography MeasurementsJournal of Tribology, 1984
- Drag minimization on a body of revolution through evolutionComputer Methods in Applied Mechanics and Engineering, 1983
- Prediction of Subsonic Aerodynamic Characteristics: A Case for Low-Order Panel MethodsJournal of Aircraft, 1982
- H-R/x/ method for predicting transitionAIAA Journal, 1981
- Design of low-drag axisymmetric shapes by the inverse methodJournal of Hydronautics, 1981
- Viscious Drag Computation for Axisymmetric Bodies at High Reynolds NumbersJournal of Hydronautics, 1979
- On the Problem of Shaping an Axisymmetric Body to Obtain Low Drag at Large Reynolds NumbersPublished by Defense Technical Information Center (DTIC) ,1975
- Shaping of axisymmetric bodies for minimum drag in incompressible flowJournal of Hydronautics, 1974
- Entrainment theory for axisymmetric, turbulent, incompressible boundary layers (Entrainment theory for incompressible turbulent boundary layer velocity and drag on bodies of revolution employed in fuselage, submersible and cowlings for propulsion design)Journal of Hydronautics, 1970