Suggested Topics within your search.
Suggested Topics within your search.
- Delta wings
- Vortices 12
- Wind tunnel tests 11
- Airplanes 10
- Leading edges 10
- Wings, Triangular 10
- Computational fluid dynamics 8
- Flow visualization 8
- Angle of attack 7
- Mach number 7
- Aerodynamic characteristics 6
- Aerodynamics 4
- Flow distribution 4
- Navier-Stokes equation 4
- Aircraft design 3
- Leading edge flaps 3
- Navier-Stokes equations 3
- Reynolds number 3
- Supersonic airfoils 3
- Supersonic flow 3
- Swept wings 3
- Vortex breakdown 3
- Vortex-motion 3
- Wind tunnel models 3
- Aerodynamic configurations 2
- Aerodynamic drag 2
- Aerodynamic loads 2
- Aerofoils 2
- Angle of attack (Aerodynamics) 2
- Blunt bodies 2
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1
Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges
Published 1996Government Document Microfilm Book -
2
Subsonic Aerodynamic characteristics of a proposed advanced manned launch system orbiter configuration /
Published 1993Online Access
Government Document eBook -
3
System identification of a vortex lattice aerodynamic model
Published 2001Connect to online resource
Connect to online resource
Government Document Microfilm Book -
4
The art of sharp-leading-edged delta wings with blowing
Published 1985Government Document Microfilm Book -
5
Equivalent longitudinal area distributions of the B-58 and XB-70-1 airplanes for use in wave drag and sonic boom calculations
Published 2011Online Access
Online Access
Government Document Electronic eBook -
6
Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel /
Published 1986Government Document Microfilm Book -
7
Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls.
Published 1964Government Document Book -
8
Prediction of lift and drag for slender sharp-edge delta wings in ground proximity /
Published 1969Online Access
Government Document eBook -
9
Flow past a flat plate with a vortex/sink combination
Published 1984Government Document Microfilm Book -
10
Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 /
Published 1985Government Document Microfilm Book -
11
Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations /
Published 1986Online Access
Government Document eBook -
12
Design and construction of a remote piloted flying wing
Published 1994Government Document Microfilm Book -
13
Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds
Published 1994Connect to online resource
Government Document Book -
14
Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
Published 1993Connect to online resource
Government Document Book -
15
Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 /
Published 1985Online Access
Government Document eBook -
16
Lee-side flow over delta wings at supersonic speeds /
Published 1985Online Access
Government Document eBook -
17
Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel /
Published 1986Online Access
Government Document eBook -
18
Research in computational fluid dynamics semiannual progress report, reporting period September 1, 1986 - February, 1987 /
Published 1987Government Document Microfilm Book -
19
Stability of streamwise vortices progress report for the period ended April 1, 1986 /
Published 1987Government Document Microfilm Book -
20
Theoretical and experimental investigation of vortex breakdown final technical report, June 1, 1985 - May 31, 1986 /
Published 1986Government Document Microfilm Book