High Speed Problems of Aircraft and Experimental Methods
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€217.00
Acceleration
Aerodynamic center
Aerodynamic drag
Aerodynamic force
Aerodynamic heating
Aerodynamics
Aeroelasticity
Aeronautics
Aerospace engineering
Age Group_Uncategorized
Age Group_Uncategorized
Aileron
Aircraft
Aircraft principal axes
Airfoil
Airframe
Airplane
Airspeed indicator
Angle of attack
Aspect ratio (aeronautics)
automatic-update
B01=Allen F. Donovan
Boundary layer
Calculation
Category1=Non-Fiction
Category=KNGV
Category=PH
Category=TRP
Chord (aeronautics)
COP=United States
Delivery_Pre-order
Dihedral (aeronautics)
Drag coefficient
Drag equation
eq_bestseller
eq_isMigrated=2
eq_nobargain
eq_non-fiction
eq_science
Flight control surfaces
Flight dynamics
Flight instruments
Flight test
Free flight (model aircraft)
High impedance
Horizontal plane
Hypersonic flight
Hypersonic speed
Hypersonic wind tunnel
Inertia coupling
Jet damping
Jet propulsion
Jet Propulsion Laboratory
Language_English
Large aircraft
Lift coefficient
Liquid-propellant rocket
Loiter (aeronautics)
Mach number
Measurement
Moment of inertia
Nozzle
PA=Temporarily unavailable
Phase lag (rotorcraft)
Pilot fatigue
Polar moment of inertia
Pressure altitude
Price_€100 and above
PS=Active
Quantity
Reynolds number
Rocket engine
Slip (aerodynamics)
softlaunch
Static pressure
Supersonic aircraft
Supersonic airfoils
Supersonic speed
Supersonic wind tunnel
Swept wing
Temperature
Time of flight
True airspeed
Turbojet
Turboprop
Wind tunnel
Wing configuration
Wing loading
Wing tip
Wing twist
Product details
- ISBN 9780691625607
- Weight: 1389g
- Dimensions: 152 x 235mm
- Publication Date: 08 Dec 2015
- Publisher: Princeton University Press
- Publication City/Country: US
- Product Form: Paperback
- Language: English
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Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. 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.
