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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1967/3/

Folder.. - Mar 05 2025 11:43:46 PM
A 20-ft-diam ribbon parachute for deployment at dynamic pressures above 400 psf. c20031024 [3].pdfA 20-ft-diam ribbon parachute for deployment at dynamic pressures above 400 psf. c20031024 [3].pdf 810KB Mar 29 2010 09:13:24 AM
Air cushion craft propulsion. c20031024 [8].pdfAir cushion craft propulsion. c20031024 [8].pdf 1239KB Mar 29 2010 09:13:24 AM
Alternate approach for aerospacecraft design sensitivities. c20031024 [2].pdfAlternate approach for aerospacecraft design sensitivities. c20031024 [2].pdf 252KB Mar 29 2010 09:13:24 AM
ASW patrol aircraft of the future. c20031024 [7].pdfASW patrol aircraft of the future. c20031024 [7].pdf 1171KB Mar 29 2010 09:13:24 AM
A Welcome to a New Journal c20031024 [1].pdfA Welcome to a New Journal c20031024 [1].pdf 91KB Mar 29 2010 09:13:24 AM
Determination of subsonic drag rise by hodograph plane analysis. c20031024 [4].pdfDetermination of subsonic drag rise by hodograph plane analysis. c20031024 [4].pdf 755KB Mar 29 2010 09:13:24 AM
Dynamic analysis of the rigid rotor system. c20031024 [7].pdfDynamic analysis of the rigid rotor system. c20031024 [7].pdf 720KB Mar 29 2010 09:13:24 AM
Equilibrium configuration and tensions of a flexible cable in a uniform flowfield. c20031024 [3].pdfEquilibrium configuration and tensions of a flexible cable in a uniform flowfield. c20031024 [3].pdf 313KB Mar 29 2010 09:13:24 AM
Erratum_ _Wing-Rotor Interactions_ c20031024 [1].pdfErratum_ _Wing-Rotor Interactions_ c20031024 [1].pdf 34KB Mar 29 2010 09:13:24 AM
Limits on minimum speed V STOL wind-tunnel tests. c20031024 [6].pdfLimits on minimum speed V STOL wind-tunnel tests. c20031024 [6].pdf 1196KB Mar 29 2010 09:13:24 AM
Linear aerodynamic theory of rotor blades. c20031024 [9].pdfLinear aerodynamic theory of rotor blades. c20031024 [9].pdf 1017KB Mar 29 2010 09:13:24 AM
Optimum Configuration of a Tethering Cable c20031024 [3].pdfOptimum Configuration of a Tethering Cable c20031024 [3].pdf 380KB Mar 29 2010 09:13:24 AM
Possibilities of drag reduction by the use of flexible skin. c20031024 [7].pdfPossibilities of drag reduction by the use of flexible skin. c20031024 [7].pdf 1073KB Mar 29 2010 09:13:24 AM
Skin-friction drag at supersonic-hypersonic speeds with transition. c20031024 [2].pdfSkin-friction drag at supersonic-hypersonic speeds with transition. c20031024 [2].pdf 312KB Mar 29 2010 09:13:24 AM
Structures cost effectiveness. c20031024 [6].pdfStructures cost effectiveness. c20031024 [6].pdf 904KB Mar 29 2010 09:13:24 AM
Subsonic-transonic-drag of supersonic inlets. c20031024 [6].pdfSubsonic-transonic-drag of supersonic inlets. c20031024 [6].pdf 720KB Mar 29 2010 09:13:24 AM
Unified performance theory for V STOL aircraft in equilibrium flight. II. c20031024 [7].pdfUnified performance theory for V STOL aircraft in equilibrium flight. II. c20031024 [7].pdf 830KB Mar 29 2010 09:13:24 AM
USAAVLABS tandem rotor airloads measurement program. c20031024 [6].pdfUSAAVLABS tandem rotor airloads measurement program. c20031024 [6].pdf 918KB Mar 29 2010 09:13:24 AM
Use of variational analysis in aerospacecraft design. c20031024 [8].pdfUse of variational analysis in aerospacecraft design. c20031024 [8].pdf 1230KB Mar 29 2010 09:13:24 AM
Wind-tunnel sonic-boom testing techniques. c20031024 [5].pdfWind-tunnel sonic-boom testing techniques. c20031024 [5].pdf 968KB Mar 29 2010 09:13:24 AM