At the NASA Ames Research Center's Dryden Flight Research Facility at Edwards Air Force Base, California, a variety of ground vibration test techniques has been applied to an assortment of new or modified aerospace research vehicles. This paper presents a summary of these techniques and the experience gained from various applications. The role of ground vibration testing in the qualification of new and modified aircraft for flight is discussed. Data are presented for a wide variety of aircraft and component tests, including comparisons of sine-dwell, single-input random, and multiple-input random excitation methods on a JetStar airplane
Experimental vibration studies were conducted on two houses to determine some of the dynamic respons...
The first comprehensive ground vibration survey was performed on the XV-15 Tiltrotor Research Aircra...
The Dryden Flight Loads Research Facility (NASA) and the associated equipment for simulating the loa...
The Dryden Flight Research Facility of NASA Ames Research Center conducted a ground vibration test o...
A ground vibration test was conducted on a Lockheed JetStar airplane that had been modified for the ...
Many parameter identification techniques have been used at the NASA Ames Research Center, Dryden Res...
A complete ground vibration and aeroelastic analysis was made of a modified version of the Grumman A...
The NASA single-seat F-16XL aircraft was modified by the addition of a glove to the left wing. Vibra...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
Vibration testing spaceflight hardware is a vital, but time consuming and expensive endeavor. Tradit...
A major phase of aerospace hardware verification is vibration testing. The standard approach for suc...
Ground vibration tests were conducted on a YF-12 airplane. To approximate a structural free-free bou...
The decoupler pylon is a passive wing/store flutter suppression device. It was modified to reduce fr...
Concepts for long-range air travel are characterized by airframe designs with long, slender, relativ...
The drones for aerodynamic and structural testing (DAST) project was designed to control flutter act...
Experimental vibration studies were conducted on two houses to determine some of the dynamic respons...
The first comprehensive ground vibration survey was performed on the XV-15 Tiltrotor Research Aircra...
The Dryden Flight Loads Research Facility (NASA) and the associated equipment for simulating the loa...
The Dryden Flight Research Facility of NASA Ames Research Center conducted a ground vibration test o...
A ground vibration test was conducted on a Lockheed JetStar airplane that had been modified for the ...
Many parameter identification techniques have been used at the NASA Ames Research Center, Dryden Res...
A complete ground vibration and aeroelastic analysis was made of a modified version of the Grumman A...
The NASA single-seat F-16XL aircraft was modified by the addition of a glove to the left wing. Vibra...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
Vibration testing spaceflight hardware is a vital, but time consuming and expensive endeavor. Tradit...
A major phase of aerospace hardware verification is vibration testing. The standard approach for suc...
Ground vibration tests were conducted on a YF-12 airplane. To approximate a structural free-free bou...
The decoupler pylon is a passive wing/store flutter suppression device. It was modified to reduce fr...
Concepts for long-range air travel are characterized by airframe designs with long, slender, relativ...
The drones for aerodynamic and structural testing (DAST) project was designed to control flutter act...
Experimental vibration studies were conducted on two houses to determine some of the dynamic respons...
The first comprehensive ground vibration survey was performed on the XV-15 Tiltrotor Research Aircra...
The Dryden Flight Loads Research Facility (NASA) and the associated equipment for simulating the loa...