General Theory of High Speed Aerodynamics

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A01=William Rees Sears
Acceleration
Aerodynamic center
Aerodynamic force
Aerodynamics
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Age Group_Uncategorized
Airfoil
Angle of attack
Approximation
Asymptotic expansion
Author_William Rees Sears
automatic-update
Big O notation
Boundary layer
Boundary value problem
Calculation
Cartesian coordinate system
Category1=Non-Fiction
Category=PH
Category=PHDT
Category=TGMF1
Coefficient
Complex plane
Compressible flow
COP=United States
Critical Mach number
Critical velocity
Cylinder (geometry)
Delivery_Delivery within 10-20 working days
Differential equation
Directional derivative
Drag coefficient
Dynamic pressure
Entropy
Epicycloid
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eq_isMigrated=2
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Equation
Equation of state (cosmology)
Equations of motion
Exponential function
First-order partial differential equation
Hodograph
Horizontal plane
Hyperbolic function
Hypersonic speed
Incompressible flow
Integral equation
Integral transform
Language_English
Lift coefficient
Lorentz transformation
Mach number
Mach wave
Mass flow
Momentum theory
Momentum transfer
Oblique shock
PA=Available
Perturbation theory
Perturbation theory (quantum mechanics)
Physical plane
Plane wave
Potential flow
Pressure coefficient
Pressure gradient
Price_€100 and above
PS=Active
Quantity
Rate of convergence
Real gas
Relative velocity
softlaunch
Speed of sound
Supersonic aircraft
Supersonic airfoils
Supersonic speed
Supersonic wind tunnel
Thermodynamic process
Transonic
Two-dimensional flow
Two-dimensional space
Velocity
Velocity potential
Viscosity
Vortex sheet
Vorticity

Product details

  • ISBN 9780691653211
  • Weight: 1247g
  • Dimensions: 152 x 235mm
  • Publication Date: 19 Apr 2016
  • Publisher: Princeton University Press
  • Publication City/Country: US
  • Product Form: Hardback
  • Language: English
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Volume VI of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: physical and mathematical aspects of high speed flows; small perturbation theory; supersonic and transonic small perturbation theory; higher order approximations; nonlinear subsonic and transonic flow theory; nonlinear supersonic steady-flow theory; characteristic methods; flows with shock waves. Originally published in 1954. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

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