Aug 302012
 

NASA has just signed a small ($100 K) study contract for a “ninja star” shaped jetliner. It would be a pointy cruciform in plan view; at low speed the longer axis would be the wing and at high speed the shorter axis would be the wing. To accomplish this, the jet engines would need to rotate 90 degrees.

Supersonic Flying Wing Nabs $100,000 from NASA

This is not an entirely new idea. In the 1970’s Boeing studied a similar concept… supersonic aircraft with single-pivot rotating wings that would present long wings for low speed and short wing for high speed.

And it goes back even further. in 1963, former German aircraft designer Richard Vogt filed a patent via Boeing for a “TWO POSITION VARIABLE SHAPED WING” based on the same idea. The patent drawings seem to show a supersonic transport.

 Posted by at 8:00 pm
Aug 242012
 

Following on the heels of the MX-1964 mockup was a mockup of the B-58 as it more or less was built. Clearly built in the same facility, what’s unclear from the photo is whether any components from the previous mockup were re-used. All the major components appear to be substantially altered, so it might have been an all-new structure, or it might have used some of the same internal supports. It would be nice if such things were able to be preserved, but mockups like this usually wind up getting turned into firewood.

 Posted by at 11:22 am
Aug 132012
 

The Convair B-58 Hustler grew out of a long series of design studies dating back to the years immediately following World War II. Early concepts called for small jet bombers carried aloft by B-36 or B-60 bombers, and would shed jet engine pods during the mission. These massively complex and expensive systems evolved over time to the somewhat more straightforward B-58 which was a single stage aircraft carrying an underslung pod containing both jet fuel and a single nuclear weapon. But even that was originally intended to be a rocket powered missile.

The B-58 evolved directly from the MX-1964 design from 1952. This is recognizably related to the B-58, but had the four jet engines in two pods rather than four, and a higher degree of integration between the pod and aircraft.

 

 Posted by at 1:48 am
Aug 022012
 

A Bell Aircraft illustration of the D188A VTOL strike fighter. This design was described in detail in Article 34, available for both download and printed.

You can download a 5.5 megabyte version of this diagram; the link is HERE. To access it, you will need to enter a username and password. The username: the first word in the body of the text on page 6 of APR issue V1N4. The password: the first word in the body of the text on page 14 of the same issue. Note that both are case sensitive.

 Posted by at 11:50 pm
Jul 282012
 

A three-view of the April 1962 configuration of General Dynamics’ TFX entry. This is very clearly the F-111, but with a few minor differences. The most obvious are the different inlets and the tail “cone.” Here, it appears that at least for the USAF version, the tail cone was meant to angle downwards… presumably forming a ventral fin to aid in stability (or perhaps aid in maneuverability).

Other design features that would change include the profiles of the dorsal and horizontal stabilizers.

 Posted by at 12:46 am
Jul 252012
 

While the December 1961 configuration of General Dynamics’ TFX proposal was quite different from what was actually built as the F-111, the April 1962 configuration was quite close, though still not final. This diagram shows both designs. The most obvious changes are for positioning of the wings further forward, and the substantial increase in size of the horizontal stabilizers.

 Posted by at 10:31 pm
Jul 232012
 

The F-111 was one of those aircraft for which a *vast* number of designs were put forth. While General Dynamics won the contract, they went through a long design development for their final design. As of December 1961, the design was clearly *almost* the F-111 as it would eventually be built, but not quite:

 Posted by at 11:39 pm
Jul 112012
 

A 1955 NACA concept for a hydrogen fueled subsonic bomber. Cruise altitude was 80,000 feet; gross weight was 150,000 pounds; wing span was 345 feet; a mission radius of 4300 miles; a payload of 15,000 pounds.

 Posted by at 8:51 pm