Development of "Skeeter" helicopter; problems successfully overcome include ground resonance troubles; design of light weight undercarriage; eliminating heterodyning torsional vibrations; obtaining satisfactory engine cooling; fatigue testing transmission; and developing blade tip HTP rocket boosters for enhancing takeoff. From paper before Helicopter Assn of Great Britain.
Rig-testing helicopters
Engineering
Engineering ; 182 , n 4734
1956
2 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1921
|Engineering Index Backfile | 1948
|FLIGHT-TESTING AMATEUR-BUILT HELICOPTERS
British Library Conference Proceedings | 2002
|Flight testing of drone helicopters
Engineering Index Backfile | 1963
|Helicopters and aeroplane-helicopters
Engineering Index Backfile | 1921
|