Nicoluer HN.700 Menestrel II

A two-seat version of Menestrel first flown in 1989. The wooden low wing Menestrel is of standard fabric covered wooden construction with a one-piece single spar wing with partly elliptical outer panels. It is available in plans only.

Gallery

Engine: VW, JPX or Limbach, 80 hp
Wing span: 7.8 m / 25 ft 7 in
Wing area: 9.8 sq.m / 105.5 sq.ft
Length: 5.30 m / 17 ft 5 in
MAUW: 510 kg
Empty weight: 290 kg
Max speed: 200 kph
Cruise speed: 187 kph / 115 mph / 100 kt
Minimum speed: 70 kph
Stall: 40 mph / 35 kt
Climb rate: 4.9 m/s
Seats: 2
Fuel consumption: 17 lt/hr
Plan price (1998): 2000 Fttc

Nicolaides Parafoil

John Nicolaides, an aeronautical engineer from San Luis Obispo, California, devised a ‘pack-away’ parafoil wing aircraft. The parafoil wing works on the same principle as the ram air steerable parachutes used by advanced skydivers: forward motion forces air into the open front of the parafoil and inflates its cells to an airfoil shape, which has all the properties (and more) of a conventional aircraft wing. The parafoil is made of high strength rip stop nylon sailcloth. A cat’s cradle of supporting lines distributes the airload.
Nicolaides maintains that the parafoil aircraft is simple to fly. There are just two controls: a rudder bar for left and right and a throttle to go up or down. Speed is 40 kph (25 mph), and the machine cannot be stalled because airspeed and angle of attack are constant. The landing run is 3 m (10 ft).
A version with a payload of 5080 kg/11,200 lb has been built.

Nicolas-Claude NC-2 Aquilon

The Nicolas-Claude NC-2 Aquilon was a single-seat touring aircraft featuring a low-wing monoplane with canard foreplanes.

In 1936, French engineer Leon Claude (Leon Claude) began designing the aircraft, using the Henri Mignet formula, where the fuselage with a low center of gravity and two tandem wings were to provide the aircraft with sufficient longitudinal stability.

Claude did not have his own funds for the construction of the aircraft, but he managed to captivate the idea of industrialist Jean Nicolas.

The NC-2 was first flown on 5 April 1937 at Auxerre. France, and only the one was built. In the same year, NC-2 took part in the so-called Prototype Tour, held in many cities in France.

Gallery

NC-2 Aquilon
Engine: 1 × Train 4T, 37 kW (50 hp)
Propeller: 2-bladed fixed-pitch
Wingspan: 7 m (23 ft 0 in)
Wing area: 14 sq.m (150 sq ft)
Length: 4.3 m (14 ft 1 in)
Empty weight: 183 kg (403 lb)
Gross weight: 410 kg (904 lb)
Maximum speed: 175 km/h (109 mph, 94 kn)
Cruise speed: 130 km/h (81 mph, 70 kn)
Stall speed: 50 km/h (31 mph, 27 kn)
Range: 850 km (530 mi, 460 nmi)
Service ceiling: 4,000 m (13,000 ft)
Wing loading: 29.2 kg/sq.m (6.0 lb/sq ft)
Seats: 1

Nicholas-Beazley Pobjoy Special / Phantom I / Wittman Phantom / Flagg Phantom / Reaver Special

The Nicholas-Beazley Pobjoy Special aka the Nicholas-Beazley Phantom I, aka the Wittman Phantom, aka the Flagg Phantom, aka the Reaver Special was a world record holding air racer of the 1930s

The Nicholas-Beazley Airplane Company had imported a Pobjoy engine with a gear reduction unit for use in its new design the Nicholas-Beazley NB3. Designer Robert T. Jones computed the weight and balance for the setup and proposed a new design as an air-racer. Claude Flagg and H. F. Landis built the aircraft in their spare time under the Marshall Aircraft Laboratories monicker and patented the wing design. The Nicholas-Beazley company conducted the tests and produced the subsequent engineering report on the machine, under the supervision of inhouse chief engineer T. A. Kirkup, who also designed most N.-B.

The fuselage is welded steel with fabric covering. The wings used an early application of lightweight aluminum construction with U shaped cantilever spars with wire bracing and fabric covering. The aircraft used wheels with small tires and without brakes. The cockpit was open and the engine was fully cowled.

The Phantom I was given an “R” license by the federal government and, piloted by Danny A. Fowlie of Morris, Illinois, was entered in the 1930 National Air Races in Chicago from August 23 to September 1.

In 1932 Ownership passed to Air Racer Steve Wittman. A Air Commerce inspector fronted the money, and had Wittman race the aircraft to avoid a conflict of interest. The Pobjoy Special is the only racer Wittman raced that he did not build or design himself. In 1932 the Pobjoy P engine was replaced with a Pobjoy R of 75 hp. The cockpit was also enclosed. In 1933 Wittman lengthened the fuselage by 21 inches, removed the engine cowling and modified the rudder (now called the Pobjoy Special). In 1946 The engine was replaced with a Continental C-85.

In 1937 the Pobjoy Special was flipped on its back. It was rebuilt sold, and stored until the end of WWII. It resurfaced in 1948 as the Reaver Special midget racer, with a 22′ wing and the more powerful 85 hp Continental engine. John Reaver entered the aircraft as the Reaver Special in the new Goodyear Formula One races.

1930 National Air Races – Registered as R1W, pilot Danny Fowlie reached 115 mph placing third in class with a mismatched prop.

1933 Chicago International Air Races – Pilot Steve Wittman wins all races in the 200ci class with a maximum speed of 120 mph.

1934 New Orleans – Wittman wins the 100 km world speed record of 137.513 mph for aircraft less than 440 pounds.

1934 Cleveland Air Races – Wittman wins all races in the 200ci class with a speed of 129.440 mph.

1935 Cleveland Air Races – New owner Percy V. Chaffee wins all races in 200ci class.

In 1936 the 200ci class is eliminated, making the Pobjoy Special obsolete for racing.

1937 St.Louis – Last race of the Pobjoy Special.

Replica:
Turner / Repeat Aviation Nicholas-Beazley Pobjoy Special

Specifications:

Phantom I
Engine: 65 hp Pobjoy P (Niagara II)
Wingspan: 21′ 9″
Length: 12′ 9″ in
Empty weight: 355 lb
Top speed: 200+ mph

Pobjoy Special
Engine: 1 × Pobjoy R Niagara II Radial, 65 hp (48 kW)
Length: 21 ft 9 in (6.63 m)
Empty weight: 355 lb (161 kg)
Capacity: 1

Reaver Special
Engine: 85 hp Continental
Wing span: 22′

Nicholas-Beazley NB-8 / NB-8G / NG-8G / NM-8G

NB-8G

The NB-8 was a light parasol wing monoplane designed by Tom Kirkup and built by the Nicholas-Beazley Airplane Company at its factory in Marshall, Missouri. The first of 58 examples flew in 1931, and most are powered by the Armstrong-Siddeley Genet Mark II engine of 80 hp (60 kW). Initially a 36 hp Aeronca two-cylinder engine powered the aircraft, subsequently a 45 hp Szekely engine was fitted, while the final choice was an 80 hp Armstrong Siddeley Genet Mk.II. Some were later fitted with the 80 hp (60 kW) Lambert engine.

The aircraft has a high strut-mounted parasol wing that can be folded to reduce hangarage space required and to permit towing by road. The two crew seats are arranged side-by-side. Initially the cockpit was open, but some examples later had an enclosure fitted.

The NB-8G was advertised for sale at $1,790. The ‘G’ in the designation originally indicated installation of the A-W Genet radial engine. It was fully aerobatic. 58 examples were purchased, mainly by private pilot owners in the United States. Production ceased in 1935. The 58 aircraft of the type produced were: 1 NB-8, 54 NB-8G’s, 1 NG-8G, and 2 NM-8G’s.

Six examples were still extant in 2009, with at least two being fully airworthy. Examples of these can be viewed at the Old Rhinebeck Aerodrome museum in New York State, and the Historic Aircraft Restoration Museum at Creve Coeur airfield near St Louis Missouri.

N576Y (cn K-18) 1931-built single-seat parasol-winged light aircraft maintained airworthy at Old Rhinebeck. The aircraft is exhibited with its wings folded.

Gallery

NB-8G
Engine: 1 × Armstrong-Siddeley Genet II, 80 hp (60 kW)
Wingspan: 37 ft 6 in (11.43 m)
Length: 20 ft 3 in (6.17 m)
Useful load: 493 lb (224 kg)
Maximum speed: 110 mph (177 km/h)
Cruise speed: 83 mph
Stall speed: 40 mph (64 km/h)
Range: 400 miles (644 km)
Service ceiling: 18,000 ft (5,486 m)
Seats: 2

Production:
Registr. Type c/n
NC436V NB-8 K-1
NC502Y NB-8G K-2
NC517Y NM-8G K-3
NC525Y NB-8G K-4
NC524Y NB-8G K-5
NC541Y NB-8G K-6
NC542Y NB-8G K-7
NC543Y NB-8G K-8
NC544Y NB-8G K-9
NC545Y NB-8G K-10
NC558Y NB-8G K-11
NC559Y NB-8G K-12
NC560Y NB-8G K-13
NC561Y NB-8G K-14
NC562Y NB-8G K-15
NC574Y NB-8G K-16
NC575Y NB-8G K-17
NC576Y NB-8G K-18
NC577Y NB-8G K-19
NC578Y NB-8G K-20
NC580Y NB-8G K-21
NC581Y NB-8G K-22
NC582Y NB-8G K-23
NC583Y NB-8G K-24
NC584Y NB-8G K-25
NC11063 NB-8G K-26
NC11064 NB-8G K-27
NC11065 NB-8G K-28
NC11066 NB-8G K-29
NC11067 NB-8G K-30
NC11071 NB-8G K-31
NC11072 NB-8G K-32
NC11073 NB-8G K-33
NC11074 NB-8G K-34
NC11075 NB-8G K-35
NC11087 NB-8G K-36
NC11088 NB-8G K-37
NC11089 NB-8G K-38
NC11090 NB-8G K-39
NC11091 NG-8G K-40
NC11095 NB-8G K-41
NC11096 NB-8G K-42
NC11097 NB-8G K-43
NC11098 NB-8G K-44
NC11099 NB-8G K-45
NC12505 NB-8G K-46
NC12506 NB-8G K-47
NC12507 NB-8G K-48
NC12508 NB-8G K-49
NC12509 NB-8G K-50
NC12510 NB-8G K-51
NC12514 NB-8G K-52
NC12515 NB-8G K-53
NC12516 NB-8G K-54
NC12517 NB-8G K-55
NC12518 NM-8G K-56
NC12527 NB-8G K-57
NC15498 NB-8G K-58

Nicolas Salamanca

Francois Nicolas’ only design was sponsored by Marquis de Salamanca. An automobile-body-builder in Biarritz, Nicolas based his monoplane on the Antoinette, but made his even bigger. The triangular-section fuselage was long and slender, about one meter deep. Fully covered, it carried a long triangular tailplane and elevator. The rectangular wings were of dramatic seagull shape and supported by six kingposts and a forest of brace-wires.

The aeroplane is reported to performed “careful hops” on the Biarritz airfield, France, in 1910.