The Prediction of Helicopter Rotor Hover Performance using a ...
The Prediction of Helicopter Rotor Hover Performance using a ...
The Prediction of Helicopter Rotor Hover Performance using a ...
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No. Author<br />
1 H.H. Pearcey<br />
P.G. Wilby<br />
M.J. Riley<br />
P. Brotherhood<br />
REFERENCES<br />
Title, etc.<br />
<strong>The</strong> derivation and verification <strong>of</strong> a new rotor pr<strong>of</strong>ile<br />
on the basis <strong>of</strong> flow phenomena, aer<strong>of</strong>oil research and<br />
flight tests.<br />
Paper 16 in <strong>The</strong> aerodynamics <strong>of</strong> rotary wings,<br />
AGARD CP 111 (19 72)<br />
W.Z. Stephniewski Basic aerodynamics and performance <strong>of</strong> the helicopter.<br />
D.R. Clarke<br />
A.C. Leiper<br />
A.J. Landgrebe<br />
A.J. Landgrebe<br />
J.B. Rorke<br />
CD. Wells<br />
J.L. Tangier<br />
R.M. Wohlfeld<br />
S.J. Miley<br />
R.A. Piziali<br />
F.A. Du Waldt<br />
P. Brotherhood<br />
D.W. Brown<br />
Paper 2 in <strong>Helicopter</strong> aerodynamics and dynamics,<br />
AGARD LS 63 (19 73)<br />
<strong>The</strong> free wake analysis - a method for the prediction<br />
<strong>of</strong> helicopter rotor hovering performance.<br />
Journ. American <strong>Helicopter</strong> Soc, \5_, No.l, 3-11, (1970)<br />
An analytical method for predicting rotor wake geometry.<br />
Journ. American <strong>Helicopter</strong> Soc, _U, No.4, 20-32, (1969)<br />
An analytical and experimental investigation <strong>of</strong> heli<br />
copter rotor hover performance and wake geometry<br />
characteristics.<br />
USA AMRDL Technical Report 71-24 (1971)<br />
<strong>The</strong> prescribed wake momentum analysis.<br />
Proceedings <strong>of</strong> the 3rd CAL/AVLABS Symposium on Aerodyna<br />
mics <strong>of</strong> rotary wings and V/STOL aircraft, Vol.1,<br />
Cornell Aeronautical Lab Inc., Buffalo, New York,<br />
June 1969<br />
An experimental investigation <strong>of</strong> vortex stability, tip<br />
shapes, compressibility and noise for hovering model<br />
rotors .<br />
NASA CR 2305 (19 73)<br />
A method <strong>of</strong> computing rotary wing airload distribution<br />
in forward flight.<br />
CAL Report BB-1495-S-1 (1962)<br />
RAE Technical Report to be published.<br />
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