1969
DOI: 10.1002/jps.2600580422
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Influence of Formulation on Aerosol Particle Size

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1969
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Cited by 69 publications
(15 citation statements)
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“…Increased vapor pressure has been correlated with decreases in particle-size output from MDIs. 7,10 Higher vapor pressure results in greater mechanical disruption of the propellant during actuation, and greater evaporation rate of the propellant droplets. 14 The MDIs produced plumes similar to those produced by commercial MDI products (Figure 1).…”
Section: Effect Of Propellant Composition On the Mmad Gsd And Fpf Omentioning
confidence: 99%
“…Increased vapor pressure has been correlated with decreases in particle-size output from MDIs. 7,10 Higher vapor pressure results in greater mechanical disruption of the propellant during actuation, and greater evaporation rate of the propellant droplets. 14 The MDIs produced plumes similar to those produced by commercial MDI products (Figure 1).…”
Section: Effect Of Propellant Composition On the Mmad Gsd And Fpf Omentioning
confidence: 99%
“…34 Although the size of aerosol particles with mesh nebulizers varies, 44,45 a significant proportion are Ͻ 3.3 m. 45,46 The vapor pressure of the propellant mixture, ambient temperature, design of the valve stem and actuator orifice, and drug concentration affect aerosol particle size produced from the pMDI. 47,48 For example, high vapor pressure of propellants generates finer aerosol particles, whereas a higher drug concentration increases the size of aerosol particles produced from the pMDI.…”
Section: Effect Of Particle Sizementioning
confidence: 99%
“…The mechanism responsible for droplet generation from bulk formulation is known to be transient, turbulent, and highly complex (Finlay 2001). Early experimental work by Polli et al (1969) identified key factors affecting the particle size of pMDI aerosols: propellant vapor pressure and spray orifice size, as well as drug particle size, drug concentration, and presence of surfactant in the suspension formulation. Fletcher (1975) studied steady flows of flashing mixtures of CFC propellants 11, 12, and 114 through a twin-orifice system.…”
Section: Introductionmentioning
confidence: 99%