[go: up one dir, main page]

Storkmann et al., 1998 - Google Patents

Force measurements in hypersonic impulse facilities

Storkmann et al., 1998

Document ID
9689038202719955851
Author
Storkmann V
Olivier H
Gronig H
Publication year
Publication venue
AIAA journal

External Links

Snippet

FORCE measurements in high-enthalpy wind tunnels are re-stricted by the short duration the steady flowfield can be sustained. Typical values for the flow duration achieved range from 0.5 to 10 ms. Because of the sudden impact of the aerodynamic forces on the model …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06Measuring arrangements specially adapted for aerodynamic testing
    • G01M9/062Wind tunnel balances; Holding devices combined with measuring arrangements
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02Wind tunnels
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
    • G01M7/00Vibration-testing of structures; Shock-testing of structures
    • G01M7/08Shock-testing
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
    • G01M5/00Investigating the elasticity of structures, e.g. deflection of bridges, air-craft wings
    • G01M5/0041Investigating the elasticity of structures, e.g. deflection of bridges, air-craft wings by determining deflection or stress
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/30Investigating strength properties of solid materials by application of mechanical stress by applying a single impulsive force, e.g. by falling weight
    • G01N3/313Investigating strength properties of solid materials by application of mechanical stress by applying a single impulsive force, e.g. by falling weight generated by explosives
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values

Similar Documents

Publication Publication Date Title
Storkmann et al. Force measurements in hypersonic impulse facilities
Mee et al. Three-component force balance for flows of millisecond duration
Steinle et al. Wind tunnel flow quality and data accuracy requirements
US3019643A (en) Strain gauge balances
Li et al. Force measurement and support integrated device in hypersonic wind tunnel
Li et al. A new airframe/propulsion-integrated aerodynamic testing technology in hypersonic wind tunnel
Sahoo et al. Dynamic force balances for short-duration hypersonic testing facilities
Liu et al. Suspension force measuring system for hypersonic wind tunnel test: Design and tests
Shaw et al. Full-scale flight demonstration of active control of a pod wake
Allegre et al. Experimental rarefied aerodynamic forces at hypersonic conditions over 70-degree blunted cone
Rivera et al. Experimental flutter boundaries with unsteady pressure distributionsfor the NACA 0012 benchmark model
Takahashi et al. Development of a new force measurement method for scramjet testing in a high enthalpy shock tunnel
Burt et al. Effect of sting oscillations on the measurement of dynamic stability derivatives
Burt A Description of a Pitch/Yaw Dynamic Stability, Forced-Oscillation Test Mechanism for Testing Lifting Configurations
Paris et al. Measurement of the aerodynamic coefficients of re-entry vehicles in short duration hypersonic facilities
Garçon et al. Unsteady load measurements on the main engine nozzle of the Ariane 5 launch vehicle
DANSBERRY Dynamic characteristics of a Benchmark models program supercritical wing
Beyers Direct derivative measurements in the presence of sting plunging
Smolinski Proof of concept for testing acceleration compensation force balance techniques in short duration flows with a CEV capsule
Davis Jr et al. Buffet tests of an attack-airplane model with emphasis on analysis of data from wind-tunnel tests
Uselton et al. Critical Sting Length as Determined by the Measurement of Pitch-Damping Derivatives for Laminar, Transitional, and Turbulent Boundary Layers at Mach Number 3 for Reduced Frequencies of 0.0033 and 0.0056
Paris et al. Semi-free oscillation method for dynamic stability characterization on re-usable launcher first-stage
Tapscott Some static longitudinal stability characteristics of an overlapped-type tandem-rotor helicopter at low airspeeds
Mineck Reynolds number effects on the performance of ailerons and spoilers
Bugeau et al. Hermes first force measurement in ONERA-F4 wind tunnel