Airfoil shape for flight at subsonic speeds
Abstract
An airfoil having an upper surface shaped to control flow accelerations and pressure distribution over the upper surface and to prevent separation of the boundary layer due to shock wave formulation at high subsonic speeds well above the critical Mach number. A highly cambered trailing edge section improves overall airfoil lifting efficiency.
- Inventors:
-
- Hampton, VA
- Publication Date:
- Research Org.:
- Sandia National Laboratories (SNL), Albuquerque, NM, and Livermore, CA (United States)
- OSTI Identifier:
- 862509
- Patent Number(s):
- US 3952971
- Assignee:
- United States of America as represented by Administrator of (Washington, DC)
- DOE Contract Number:
- AC04-76
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- airfoil; shape; flight; subsonic; speeds; upper; surface; shaped; control; flow; accelerations; pressure; distribution; prevent; separation; boundary; layer; due; shock; wave; formulation; critical; mach; highly; cambered; trailing; edge; section; improves; overall; lifting; efficiency; pressure distribution; wave form; upper surface; shock wave; trailing edge; boundary layer; control flow; surface shaped; surface shape; /244/
Citation Formats
Whitcomb, Richard T. Airfoil shape for flight at subsonic speeds. United States: N. p., 1976.
Web.
Whitcomb, Richard T. Airfoil shape for flight at subsonic speeds. United States.
Whitcomb, Richard T. 1976.
"Airfoil shape for flight at subsonic speeds". United States. https://www.osti.gov/servlets/purl/862509.
@article{osti_862509,
title = {Airfoil shape for flight at subsonic speeds},
author = {Whitcomb, Richard T},
abstractNote = {An airfoil having an upper surface shaped to control flow accelerations and pressure distribution over the upper surface and to prevent separation of the boundary layer due to shock wave formulation at high subsonic speeds well above the critical Mach number. A highly cambered trailing edge section improves overall airfoil lifting efficiency.},
doi = {},
url = {https://www.osti.gov/biblio/862509},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Thu Jan 01 00:00:00 EST 1976},
month = {Thu Jan 01 00:00:00 EST 1976}
}
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