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THE LOCKHEED BLC HERCULES A PRACTICAL STOL TRANSPORT
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DICKERMAN, F. and BRANSON, C., "THE LOCKHEED BLC HERCULES A PRACTICAL STOL TRANSPORT," SAE Technical Paper 600455, 1960, https://doi.org/10.4271/600455.Also In
References
- Department of the Air Force letter “General Operational Requirement for a Troop Carrier Assault Aircraft (Fixed Wing) Support System” GOR No. 130 February 1958
- Weiberg J. A. Page V. R. “Large-Scale Wind-Tunnel Tests of an Airplane Model with an Unswept, Aspect-Ratio 10-Wing, Four Propellers, and Blowing Flaps” NASA Technical Note D-25 September 1959
- Schwartzberg M. A. “Analysis of Wind Tunnel Test Results Obtained for a Propeller-Powered Model with Flap Blowing” Martin Engineering Report 9429 August 1957
- Military Specification “Flying Qualities of Piloted Airplanes” MIL-F-8785 (ASG) October 1954
- Fasano A. Balch R. “Wind-Tunnel Tests of a Lockheed GL-128 Airplane Model” United Aircraft Corp. Research Department Report R-1546 12 October 1959
- Kuhn R. Naeseth R. “Tunnel-Wall Effects Associated with VTOL-STOL Model Testing” Langley Research Center, Langley Field, Va. Presented at the Meeting of the Wind Tunnel and Model Testing Panel Advisory Group for Aeronautical Research and Development, NATO March 1959
- Wallace R. E. “Systematic Two-Dimensional Tests of an NACA 23015 Airfoil Section with a Single-Slotted Flap and Circulation Control” University of Wichita Aeronautical Report 120 August 1954