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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 />

29

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