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Full-scale Aircraft Simulation with Cryogenic Tunnels and Status of the National Transonic Facility

Full-scale Aircraft Simulation with Cryogenic Tunnels and Status of the National Transonic Facility PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

Book Description


Full-scale Aircraft Simulation with Cryogenic Tunnels and Status of the National Transonic Facility

Full-scale Aircraft Simulation with Cryogenic Tunnels and Status of the National Transonic Facility PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

Book Description


Airborne Lidar Experiments at the Savannah River Plant

Airborne Lidar Experiments at the Savannah River Plant PDF Author: William B. Krabill
Publisher:
ISBN:
Category : Aerial photographs in botany
Languages : en
Pages : 776

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340

Book Description


Simulation of Flight Test Conditions in the Langley Pilot Transonic Cryogenic Tunnel

Simulation of Flight Test Conditions in the Langley Pilot Transonic Cryogenic Tunnel PDF Author: Robert A. Kilgore
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 28

Book Description
The theory and advantages of the cryogenic tunnel concept are briefly reviewed. The unique ability to vary temperature independently of pressure and Mach number allows, in addition to large reductions in model loads and tunnel power, the independent determination of Reynolds number, Mach number, and aeroelastic effects on the aerodynamic characteristics of the model. Various combinations of Reynolds number and dynamic pressure are established to represent accurately flight variations of aeroelastic deformation with altitude changes. The consequences of the thermal and caloric imperfections of the test gas under cryogenic conditions were examined and found to be insignificant for operating pressures up to 5 atm. The characteristics of the Langley pilot transonic cryogenic tunnel are described and the results of initial tunnel operation are presented. Tests of a two-dimensional airfoil at a Mach number of 0.85 show identical pressure distributions for a chord Reynolds number of 8,600,000 obtained first at a stagnation pressure of 4.91 atm at a stagnation temperature of 322.0 K and then at a stagnation pressure of 1.19 atm at a stagnation temperature of 116.5 K.

Cryogenic Wind Tunnels

Cryogenic Wind Tunnels PDF Author: Marie H. Tuttle
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 76

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 240

Book Description


Cryogenic Wind Tunnels: A Comprehensive, Annotated Bibliography

Cryogenic Wind Tunnels: A Comprehensive, Annotated Bibliography PDF Author: Marie H. Tuttle
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 146

Book Description


Cryogenic Wind Tunnels

Cryogenic Wind Tunnels PDF Author: Marie H. Tuttle
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 96

Book Description


Wind-tunnel/flight Correlation, 1981

Wind-tunnel/flight Correlation, 1981 PDF Author: L. Wayne McKinney
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 244

Book Description


NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 510

Book Description