Boulton-Paul P.111
1950
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Boulton-Paul P.111

The Boulton Paul P.111 and P.120 delta wing research aircraft, built to Air Ministry Specification E.27/46 and E.27/49 respectively, were used to investigate high speed characteristics of the delta wing.

The P.111 flew in October 1950, powered by a Rolls-Royce Nene turbojet. Its delta wing had a leading-edge sweep of 45, and detachable wingtips made it easy to carry out comparative tests with blunt and pointed tips. The fin tip was similarly detachable, and there was no tailplane.

After tests in its original form, the aircraft was fitted with a nose probe and four rectangular airbrakes around the front fuselage. Some internal modifications were also made and in this new form it received the designation P.111 A, recommencing flight tests in July 1953. It could attain level speeds in the region of Mach 0.95-0.98, and become supersonic in a shallow dive. The P.111A survives in the Midland Air Museum at Coventry's Baginton Airport.

3-View 
Boulton-Paul P.111A three-view drawing (800 x 500)


Specification 
 MODELP.111A
 CREW1
 ENGINE1 x Rolls Royce "Nene", 2313kg
 WEIGHTS
    Take-off weight4354 kg9599 lb
    Empty weight2948 kg6499 lb
 DIMENSIONS
    Wingspan10.21 m34 ft 6 in
    Length7.95 m26 ft 1 in
    Height3.82 m13 ft 6 in
    Wing area18.58 m2199.99 sq ft
 PERFORMANCE
    Max. speed0.98M0.98M

Boulton-Paul P.111

Comments
Bob Jaffray, 01.03.2007

Your outline of the BP Delta is very brief and thus misses the critical feature, that of total hydraulic, irreversible, powered flying controls. Artificial feel for the pilot was by way of built in springs which could not be fully trimmed to take into account the very fine degree of control necessary, particularly with the minimal input demanded at high IAS. The design work was carried out at Farnborough, and all of the early flying was by Aero Flight pilots including Bob Smythe CO, Jim Harrison, and Jock Elliot. Jock carried out most of the flying with 52 flights totalling some 26 hours. He it was who, commenting on the sensitivy of the controls at IAS, stated that, at 500 kts IAS, 1/4" stick movement gave 1"g" of acceleration, and observed that the possibility of a strong reflex input was very real and would have catastrophic results. Following a belly landing by Jim Harrison the design was near to being shelved, when Jock came up with the idea for variable gearing between stick and surfaces; this facility would be available to the pilot in flight and would allow a choice ranging between 1:1 to 4:1. Jock pointed out that the idea was not new and that some of the Schneider Trophy aircraft had incorporated the idea.
The idea was discussed at a meeting with Dennis Higton, aerodynamicist at RAE, JD North of BP, and Jock, and the outcome was that it was incorporated into the design, now known as the BP P111a.
The point has been made (Dave Morgan) that Jock's concept of variable gearing was an crital break through for the aviation industry and virtually paved the way for Concorde and all high speed aircraft that followed.
Ben Gunn flew the aircraft in it's later form of P111a.
The Delta was a significant, and brave, design at a time when even swept wings were viewed with some trepidation, and the delta was truly futuristic; the variable gearing was crtitical in the design of all high speed flying from that point on.
I hope these notes add to you knowl...

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