NATURAL LAMINAR FLOW FLIGHT EXPERIMENTS ON A SWEPT WING BUSINESS JET-BOUNDARY LAYER STABILITY ANALYSIS Contractor
- Author(s):
- Rozendaal, R.A. ( Boeing Commercial Airplane Co. )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1986
- Issue:
- NASA-CR-3975
- No.:
- G3/02 43057
- Pt.:
- NAS1.26:3975
- Paper no.:
- N86-24659
- Page(from):
- 1
- Page(to):
- 98
- Pages:
- 98
- Pub. info.:
- National Aeronautics and Space Administration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
F-111 NATURAL LAMINAR FLOW GLOVE FLIGHT TEST DATA ANALYSIS AND BOUNDARY LAYER STABILITY ANALYSIS Contractor
National Aeronautics and Space Administration |
7
Technical Paper
Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Large-eddy simulation of laminar-turbulent transition in a swept-wing boundary layer
American Institute of Aeronautics and Astronautics |
"Society of Automotive Engineering, Inc." |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Variavle Sweep Transition Flight Experiment(VSTFE) ― Unified Stability System (USS) Description and User's Manual
National Aeronautics and Space Adminstration |
5
Technical Paper
Effects of Wing Sweep on In-Flight Boundary-Layer Transition for a Laminar Flow Wing at Mach Numbers From 0.60 to 0.79
National Aeronautics and Space Adminstration |
11
Technical Paper
DNS of Attachment-line/Crossflow Boundary Layer Instability in Supersonic Swept Wing Flows
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Experiments in nonlinear saturation of stationary crossflow vortices in a swept-wing boundary layer
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |