Results 101 to 110 of about 2,840 (207)

Preliminary study of VTO thrust requirements for a V/STOL aircraft with lift plus lift/cruise propulsion [PDF]

open access: yes
A preliminary assessment was made of the VTO thrust requirements for a supersonic (Type B) aircraft with a Lift plus Lift/Cruise propulsion system. A baseline aircraft with a takeoff gross weight (TOGW) of 13 608 kg (30,000 lb) was assumed.
Allen, J. L., Turney, G. E.
core   +1 more source

Conceptual design, evaluation and research identification for Remote Augmented Propulsive Lift Systems (RALS) with ejectors for VTOL aircraft [PDF]

open access: yes
Ejector concepts for use with a remote augmented lift system (RALS) exhaust nozzle were studied. A number of concepts were considered and three were selected as having the greatest promise of providing the desired aircraft and exhaust gas cooling and ...
Konarski, M.   +2 more
core   +1 more source

On the passive limited slip differential for high performance vehicle applications [PDF]

open access: yes
The paper is aimed at a comprehensive revision of the working principles and limitations of the mechanical limited slip differential, the traditional, passive device used to improve traction capabilities and to extend the performance envelope of high ...
Chindamo, Daniel   +2 more
core  

Hummingbirds use wing inertial effects to improve manoeuvrability. [PDF]

open access: yesJ R Soc Interface, 2023
Haque MN, Cheng B, Tobalske BW, Luo H.
europepmc   +1 more source

Attitude Control for an Aero-Vehicle Using Vector Thrusting and Variable Speed Control Moment Gyros [PDF]

open access: yes
Stabilization of passively unstable thrust-levitated vehicles can require significant control inputs. Although thrust vectoring is a straightforward choice for realizing these inputs, this may lead to difficulties discussed in the paper.
Lim, K. B.   +2 more
core   +1 more source

Conceptual design study report [PDF]

open access: yes
Conceptual design of Northrop V/STOL jet operations research supersonic ...

core   +1 more source

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