SEARCH · Search NASA

Results for “V/STOL”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

SourceResearch connectionFrom yearThrough year

Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.

At least 127 records · Page 7

All sources NASA NTRS DOE OSTI

NASA NTRS1964

Dynamic Tests of V/STOL Transport Models

This paper presents a summary of results obtained in dynamic tests of free-flight models of various configurations suitable for V/STOL transport aircraft at the NASA Langley Research Center. The configurations covered will be the tilt-wing propeller-driven type as represented by the XC-142A tri-service transport, the fan-in-wing type as represented by the XV-5A research airplane, and the jet-lift type as represented by the Dornier 00-31 transport. The test techniques themselves are not described in this paper since they have been described in detail previously in references 1 and 2.

Dynamic stability↗

NASA NTRS1964

Flight investigation of stability and control characteristics of a 1/9-scale model of a four-propeller tilt-wing v/stol transport

Stability & control of 4-propeller, tilt-wing v/stol scale model transport aircraft

STABILITY AND CONTROL↗

NASA NTRS1964

Effects of gross changes in static directional stability on v/stol handling characteristics based on a flight investigation

Helicopter flight investigation of effects of gross changes in static directional stability on v/stol handling

HELICOPTER↗

NASA NTRS1964

Aerodynamics and flying qualities of jet v/stol airplanes.

Jet v/stol aircraft aerodynamics and flying qualities summarized

PROPULSION SYSTEM PERFORMANCE↗

NASA NTRS1964

Dynamic tests of v/stol transport models

Dynamic tests of free flight models of various configurations for V/STOL transport aircraft

DYNAMIC MODEL↗

NASA NTRS1965

V/stol plenum chamber combustion research study, phase i final report

V/STOL plenum chamber design for combustion system efficiency in fan duct of turbofan engine

V/STOL AIRCRAFT↗

NASA NTRS1965

V/stol characteristics in relation to terminal requirements

Terminal and support facilities required by V/STOL aircraft for use as air transportation

GROUND SUPPORT SYSTEM↗

NASA NTRS1964

Status of v/stol research and development in the united states.

Current research and development of V/STOL AIRCRAFT

AIRCRAFT DESIGN↗

NASA NTRS1964

Simulation techniques for the study of V/STOL PROBLEMS

Simulation techniques for study of V/STOL AIRCRAFT problems - cockpit, control, motion, and display requirements

COCKPIT SIMULATOR↗

NASA NTRS1965

An experimental investigation of feasibility of a V/STOL test section in UWAL 8 x 12 wind tunnel by using a 1/8 scale model of the tunnel

Feasibility of V/STOL test section in wind tunnel by using one eighth scale model of tunnel

SCALE MODEL↗

NASA NTRS1966

Experimental and Theoretical Investigation of Wind Tunnel Geometry, Emphasizing Factors Pertinent to V/STOL Vehicles Testing Progress Report No. 2, Mar. 16 - Sep. 15, 1965

Powered rotor installation, tunnel internal flow analysis using vortex ring, and flow field calculation of highly loaded systems in free air for V/STOL vehicles test program

VORTEX RING↗

NASA NTRS1960