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Posts
- Category: THEORETICAL AERODYNAMICS (continued)
- Category: Theoretical and Applied Aerodynamics
- Special Techniques
- Equilibrium of the Glider
- Induced Velocity
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium Condition and Static Stability
- Equilibrium of the AMAT11
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium Condition and Static Stability
- Equilibrium of the AMAT2010
- . Including Twist
- Prandtl Lifting Line Theory
- Supersonic Flow (Mo > 1, в = JM( — 1)
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium of the AMAT09
- Prandtl Lifting Line Theory
- Supersonic Flow (Mo > 1, в = yjM^ — 1)
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium of the Aggie Micro Flyer
- Induced Downwash in Manoeuvre
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium of the Aggie Micro Flyer (AMF III)
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium of the Aggie Micro Flyer
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Glider Equilibrium
- Supersonic Linearized Theory (Mo > 1)
- Thin Airfoil Theory (2-D Inviscid Flow)
- Airplane Longitudinal Equilibrium
- Lifting Line Theory (3-D Inviscid Flow)
- . Thin Airfoil Theory (2-D Inviscid Flow)
- Equilibrium of the Glider (3-D Incompressible Flow)
- Lifting Line Theory
- Equilibrium About an Axis
- Solutions to Problems
- Equilibrium of the Glider
- Induced Velocity
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium of the AMAT11
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium of the AMAT10
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium of the AMAT09
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium of the Aggie Micro Flyer
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Equilibrium Incidence
- Equilibrium of the Aggie Micro Flyer
- Prandtl Lifting Line Theory
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Take-Off Conditions
- Equilibrium of the Aggie Micro Flyer
- Prandtl Lifting Line Theory
- Supersonic Flow (M0 > 1, в = JM(2 — 1)
- 2-D Inviscid, Linearized, Thin Airfoil Theories
- Glider Equilibrium
- Lifting Line Theory (3-D Inviscid Flow)
- Thin Airfoil Theory (2-D Inviscid Flow)
- Airplane Longitudinal Equilibrium
- Lifting Line Theory (3-D Inviscid Flow)
- Problem 2
- Equilibrium of the Glider (3-D Incompressible Flow)
- Lifting Line Theory
- Problems
- Electronic Analog Computers: Networks Versus Tanks
- Sobieczky’s Rheograph-Transformations
- Analog Study of Three-Dimensional Flows
- Analog Study of Supersonic Conical Flows
- Д дф д дф дх р'дх + дг '"Hr = 0 (13.61) and д Щ - + д = 0 дх рг дх дг рг дг (13.62) These equations can be compared to the equations governing the electrical potential in a conducting medium of varying thickness. The depth of the conducting material will be proportional or inversely proportional to рг, depending on whether ф or ф is simulated. In the first case, inclined tank can be used to simulate flow around streamlined bodies of revolution, convergent wind tunnel ducts and axially symmetric air intakes. For the representation of the stream function, a tank with hyperbolic bottom can be constructed where the depth varies as 1/y, see Ref. [12]. 13.3.3 Hodograph Tank In the hodograph plane, the velocity potential ф and the stream function ф, of compressible fluid flow are related by the following equations д 1 дф д ( р дф дд ррд (1 - M2) дд + дв р0д дв ° (13.65) and (13.66)  
- Analog Representation of Circulation Around Lifting Airfoils
- Electric Analogy
- Hydraulic Analogy
- Flow Analogies
- Hypersonic Vehicle Design
- Hypersonic Similitude
- Hypersonic Area Rule
- Theoretical Developments
- Strong Viscous/Inviscid Interaction
- Weak Viscous/Inviscid Interactions
- Solutions of Laminar Boundary Layer Equations at Hypersonic Speeds
- Navier-Stokes Equations