Add to ORKGAnalytical method for predicting lift and drag for slender sharp-edge delta wings near ground leve
The suction analogy concept of Polhamus for predicting vortex lift in conjunction with an appropriat...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
Wind tunnel tests were conducted to determine the subsonic longitudinal aerodynamic characteristics ...
Sharp edge delta wing drag prediction by application of leading edge suction analogy of vortex lif
Slender sharp-edge wings having leading-edge sweep angles of 74 deg have been studied at Mach number...
A method of predicting forces, moments, and detailed surface pressures on thin, sharp-edged wings wi...
A semiempirical method to predict vortex breakdown effects on aerodynamic characteristics of slender...
Many types of hypersonic aircraft configurations are currently being studied for feasibility of futu...
Steady lifting flows over highly swept delta wings at large incidence were studied. After an exhaust...
In order to indicate the effects of Reynolds number and other variables on the drag due to lift of d...
A concept for the calculation of the vortex lift of sharp-edge delta wings is pre sented and compare...
The leading-edge-suction analogy of Polhamus has been used to develop the longitudinal load distribu...
A low speed investigation of the flow over a 40 degree apex angle delta wing with sharp leading edge...
A set of empirical methods was developed to predict low-speed lift, drag and pitching-moment variati...
The suction analogy concept of Polhamus for predicting vortex lift in conjunction with an appropriat...
The suction analogy concept of Polhamus for predicting vortex lift in conjunction with an appropriat...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
Wind tunnel tests were conducted to determine the subsonic longitudinal aerodynamic characteristics ...
Sharp edge delta wing drag prediction by application of leading edge suction analogy of vortex lif
Slender sharp-edge wings having leading-edge sweep angles of 74 deg have been studied at Mach number...
A method of predicting forces, moments, and detailed surface pressures on thin, sharp-edged wings wi...
A semiempirical method to predict vortex breakdown effects on aerodynamic characteristics of slender...
Many types of hypersonic aircraft configurations are currently being studied for feasibility of futu...
Steady lifting flows over highly swept delta wings at large incidence were studied. After an exhaust...
In order to indicate the effects of Reynolds number and other variables on the drag due to lift of d...
A concept for the calculation of the vortex lift of sharp-edge delta wings is pre sented and compare...
The leading-edge-suction analogy of Polhamus has been used to develop the longitudinal load distribu...
A low speed investigation of the flow over a 40 degree apex angle delta wing with sharp leading edge...
A set of empirical methods was developed to predict low-speed lift, drag and pitching-moment variati...
The suction analogy concept of Polhamus for predicting vortex lift in conjunction with an appropriat...
The suction analogy concept of Polhamus for predicting vortex lift in conjunction with an appropriat...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
Wind tunnel tests were conducted to determine the subsonic longitudinal aerodynamic characteristics ...