Add to ORKGIssued as Technical progress reports no. [1-6], and Final reports no. [1-4], Project no. E-16-61
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
The differential equations of motion for the lateral and torsional deformations of a nonlinearly twi...
The wake information from a helicopter forward flight code is coupled with two transonic potential r...
Issued as Monthly reports no. [1-7], Technical progress reports no. [1-5], Draft final report, and F...
Computer programs were developed to implement the computational scheme arising from Van Holten's asy...
The numerical practicality of a matched asymptotic expansion approach for the computation of unstead...
Issued as Status report, Report, Project, and Final reports [nos. 1-2], Project no. E-16-66
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Ti...
Issued as Annual reports [nos. 1-2], Project no. E-16-676 (includes subprojects nos. E-16-526, E-25-...
Over fifty years of contributions by NASA and the Army through rotor systems flight research were ex...
Measurements of unsteady, rotary wing air loads and time derivatives for rotor blade intersecting co...
Thesis. 1975. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.Vi...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
In recent years, the development of aerodynamic technology for rotorcraft has continued successfully...
Pressure data at 90 percent blade radius for a helicopter main rotor with RC-SC2 blade sections was ...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
The differential equations of motion for the lateral and torsional deformations of a nonlinearly twi...
The wake information from a helicopter forward flight code is coupled with two transonic potential r...
Issued as Monthly reports no. [1-7], Technical progress reports no. [1-5], Draft final report, and F...
Computer programs were developed to implement the computational scheme arising from Van Holten's asy...
The numerical practicality of a matched asymptotic expansion approach for the computation of unstead...
Issued as Status report, Report, Project, and Final reports [nos. 1-2], Project no. E-16-66
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Ti...
Issued as Annual reports [nos. 1-2], Project no. E-16-676 (includes subprojects nos. E-16-526, E-25-...
Over fifty years of contributions by NASA and the Army through rotor systems flight research were ex...
Measurements of unsteady, rotary wing air loads and time derivatives for rotor blade intersecting co...
Thesis. 1975. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.Vi...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
In recent years, the development of aerodynamic technology for rotorcraft has continued successfully...
Pressure data at 90 percent blade radius for a helicopter main rotor with RC-SC2 blade sections was ...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
The differential equations of motion for the lateral and torsional deformations of a nonlinearly twi...
The wake information from a helicopter forward flight code is coupled with two transonic potential r...