The Bell X-1 reached Mach 2.44 at 74,200 ft and the X-2 reached Mach 3.2 at 126,200 ft but they both experienced inertia coupling. It wasn’t stable controlled flight.[l]
The maximum speed of the X-1 under controlled flight was Mach 1.45 at 71,900 ft (21,000m).[l]
The Bell X-1 has a thin airfoil. From the following article.
The shapes of wings also changed to keep the air from performing as much work at high speeds as it had been expected to perform at lower speeds. A thin airfoil, for example, decreases the distance that the air must flow over the wing compared with the distance that the air travels under it and therefore reduces the speed of the air over the wing. The idea behind a thin wing is to reduce the ratio of the wing’s thickness to its “chord”—the distance from the leading to the trailing edge.
Sweeping the wing back has the same effect as reducing the ratio of thickness to chord and therefore also requires less work from the air. Since a swept wing meets the air at an angle, the distance the air must travel from the leading edge to the trailing edge of the wing is longer, and its acceleration is more gradual.
The other reason was that the flights were performed at high altitude where the air density is lower. [Density Effects on Aerodynamics forces]; [Table for air density up to 250,000ft].
Happy New Year 🙂
I think the Boeing X-32 is a development of the Harrier concept of direct lift into a LO supersonic aircraft. It has many of the same features to reduce weight. The fuselage hangs from a one piece wing like the Harrier. It has a short single inlet to reduce weight. The concept is more modular as well. It would be much easier to “hang” a UCAV variant off the same wing for example.
A lot of the technological risk of the X-32 was in the use of advanced composites, thermoplastics have matured a lot if you look at the use of thermoplastics in the A380, A350 and 787. If they had succeeded it would have meant an easy to manufacture, lightweight, low cost advanced supercritical delta wing with all the advantages of a delta wing. Strong structure, large internal fuel volume and no wing fold mechanism for the naval variant (weight). The Naval and CTOL variants can share the same wing (cost) and the STOVL variant is a clipped version of the CTOL/CV wing (high commonality). Successful delta wing naval designs include the A4 Skyhawk, Dassault Rafale and F4D Skyray. I think the X-32’s delta wing is of a more advanced design than the Eurofighter and Rafale as well.
Other good points include good all aspect stealth due to the highly swept wing and aft body design with 2D exhaust blended into the rear of the aircraft. A low thermal signature due to high engine mass flow, low drag aerodynamics and long exhaust duct. 2D thrust vectoring can also be used to trim the aircraft (low drag).
I think the F-35 is a development of the Yak-141 concept. A lot of the technological risk was in the lift system but the F-35 uses large, expensive and heavy aluminium/titanium bulkheads in its design. Aircraft weight also affects costs and the F-35 weighs more than a F-15. I don’t think it’ll be a cheap aircraft to operate. The biggest criticism of the F-35 is that the F135 engine has higher thrust to weight ratio than both the EJ200 and F119 but yet the aircraft has similar E-M to a F/A-18.
Kinematics is still important in a multirole combat aircraft especially with the advent of J-20, J-31 and PAKFA. First day of war strike can be carried out by UCAVs like the X-47B which have better range payload, loiter, lower RCS, and thermal signature and Tomahawk block IV (reprogrammable inflight via sat link).
Deployable Radio Frequency Data Backbone To Match Fiber Optic Capacity [Darpa.mil]
DARPA’s 100 Gb/s RF Backbone (100G) intends to develop a fiber-optic-equivalent communications backbone that can be deployed worldwide. The goal is to create a 100 Gb/s data link that achieves a range greater than 200 kilometers between airborne assets and a range greater than 100 kilometers between an airborne asset (at 60,000 feet) and the ground.
DARPA looks to create wireless Skynet with fiber-like, 100Gb bandwidth [Arstechnica.com]
Defense Advanced Research Projects Agency has launched a program to create technology that can act as a backbone for an airborne network with the same sort of bandwidth as fiber optic backbones—100 gigabits per second.
Truman Hosts First Flight Deck Taxiing of X-47B UCAS-D
December 9th, 2012
Sailors aboard the aircraft carrier USS Harry S. Truman (CVN 75) and personnel from the Navy Unmanned Combat Air System program office (PMA-268) integrated test team made history Dec. 9 as they taxied an X-47B Unmanned Combat Air System (UCAS) demonstrator aircraft for the first time aboard a carrier.
X-47B deck handling trials Youtube video
Photos
http://www.navy.mil/view_image.asp?id=141119
http://www.navy.mil/view_image.asp?id=141118
http://www.navy.mil/view_image.asp?id=141115
http://www.navy.mil/view_image.asp?id=141116
http://www.navy.mil/view_image.asp?id=141117
http://www.navy.mil/view_image.asp?id=141112
http://www.navy.mil/view_image.asp?id=141113
http://www.navy.mil/view_image.asp?id=141114
http://www.navy.mil/view_image.asp?id=141111
nEUROn first flight December 1st 2012 (Photo gallery)
Very excited about this news. Have been looking forward to it.
Thrust vectoring can also be used to trim the aircraft for lower drag during supersonic flight.

AW159 with Thales LMM
Beautiful aircraft. Interesting to see the 5XX Modex for heavy attack.
F-35 AMRAAM weapons separation test [Youtube link]
http://www.edwards.af.mil/news/story.asp?id=123323312
10/22/2012 – EDWARDS AIR FORCE BASE, Calif. — An F-35A conventional takeoff and landing (CTOL) aircraft completed the first in-flight weapons release of an instrumented AIM-120 from a 5th Generation fighter, Oct. 19.
The aircraft’s planform seems similar to the YF-22 but with less sweep?

It would be interesting to have an estimate of the aircraft’s dry thrust to weight ratio with a modest air to air loadout. 🙂
The rudders interact with the vortex generated by the LERX.
Youtube: Ex-Varyag returning from its 8th sea trial
China’s first aircraft carrier, the refurbished and modernized Ex-Varyag, returns from its 8th sea-trial in the Bohai Gulf on 21st June 2012 that lasted 14 days.
PICTURE: Taranis demonstrator tested, as first flight slips into 2013
The UK has delayed the first flight of its Taranis unmanned combat air system technology demonstrator until “the first part of 2013”, according to lead company BAE Systems. – Flight International