Results 161 to 170 of about 151,224 (313)

Estimation of shock layer thickness and pressure distribution on a delta wing-body space shuttle orbiter [PDF]

open access: yes
Calculation of shock inclination angle and surface pressure coefficient in vertical plane of symmetry of bodies at angle of attack related to delta wing-body space shuttle ...
Kaattari, G. E.
core   +1 more source

A Perspective of Multi‐Reflecting TOF MS

open access: yesMass Spectrometry Reviews, EarlyView.
ABSTRACT Time‐of‐flight mass spectrometry (TOF MS) excels in rapid and high‐sensitivity analysis, making it a cornerstone of analytical chemistry. But as sample complexity explodes in omics studies, so does the need for higher resolving power to ensure accurate results.
A. N. Verenchikov   +3 more
wiley   +1 more source

Analytical observations on the aerodynamics of a delta wing with leading edge flaps [PDF]

open access: yes
The effect of a leading edge flap on the aerodynamics of a low aspect ratio delta wing is studied analytically. The separated flow field about the wing is represented by a simple vortex model composed of a conical straight vortex sheet and a concentrated
Oh, S., Tavella, D.
core   +1 more source

Cold EI—The Way to Improve GC‐MS and Increase Its Range of Applications

open access: yesMass Spectrometry Reviews, EarlyView.
ABSTRACT Gas chromatography‐mass spectrometry (GC‐MS) with Cold electron ionization (EI) is based on interfacing the GC and MS with a supersonic molecular beam (SMB) along with electron ionization of vibrationally cold sample compounds in the SMB in a contact‐free fly‐through ion source (hence the name Cold EI).
Aviv Amirav   +3 more
wiley   +1 more source

Neuralized-like proteins differentially activate Notch ligands. [PDF]

open access: yesEMBO Rep
Airich A   +7 more
europepmc   +1 more source

Subsonic investigations of vortex interaction control for enhanced high-alpha aerodynamics of a chine forebody/Delta wing configuration [PDF]

open access: yes
A proposed concept to alleviate high alpha asymmetry and lateral/directional instability by decoupling of forebody and wing vortices was studied on a generic chine forebody/ 60 deg.
Bhat, M. K., Rao, Dhanvada M.
core   +1 more source

Model Predictive Filtering MR Temperature Imaging for Laser‐Induced Interstitial Thermotherapy

open access: yesMagnetic Resonance in Medicine, EarlyView.
ABSTRACT Purpose To evaluate the use of the Model Predictive Filtering (MPF) method to improve temporal resolution of magnetic resonance temperature imaging (MRTI) for monitoring laser interstitial thermal therapy (LITT) ablations. Methods Using a Green's function method for solving differential equations, a treatment‐specific power matrix Q was ...
Joshua Marchant   +3 more
wiley   +1 more source

Navier-Stokes calculation of transonic flow past the NTF 65-deg delta wing [PDF]

open access: yes
Viscous flow past a wind tunnel model of a 65-degree swept angle Delta wing at transonic speeds is being studied. The model was tested in the 8-foot cryogenic transonic wind tunnel at the National Transonic Facility.
Wu, Chivey
core   +1 more source

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