An Approach to Constrained Aerodynamic Design With Application to Airfoils
- Author(s):
- Campbell, Richard L ( Langley Research Center )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1992
- Issue:
- NASA-TP-3260
- No.:
- H1/02 0128403
- Pt.:
- NAS 1.60:3260
- Paper no.:
- N93-12321
- Page(from):
- 1
- Page(to):
- 24
- Pages:
- 24
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
8
Technical Paper
On the Aerodynamic Design of Compressor Airfoils for Robustness Under Geometric Uncertainty.
American Society of Mechanical Engineers |
National Aeronautics and Space Adminstration |
9
Technical Paper
Aerodynamic Design of Transonic Airfoils Using Simulated Annealing and Navier-Stokes Equations
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
10
Technical Paper
A Fast Aerodynamic Procedure for a Complete Aircraft Design Using the Know Airfoil Characteristics.
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
12
Technical Paper
Aerodynamic Characteristics of Two Rotorcraft Airfoils Designed for Application to the Inboard Region of a Main Rotor Blade
National Aeronautics and Space Adminstration |