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Online Books by

Vigyan Research Associates

Books from the extended shelves:

• Vigyan Research Associates: Calculation of high angle of attack aerodynamics of fighter configurations. Vol. I, Steady (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1991., 1991), also by C. Edward Lan, Ratikanta Tripathi, S. C. Mehrotra, P. Sundaram, Suei Chin, H. Emdad, Air Force Flight Dynamics Laboratory (U.S.), Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and United States. Air Force. Systems Command (page images at HathiTrust)
• Vigyan Research Associates: Calculation of high angle of attack aerodynamics of fighter configurations. Vol. II, User manual for VORSTAB-II (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1991., 1991), also by C. Edward Lan, Ratikanta Tripathi, S. C. Mehrotra, P. Sundaram, Suei Chin, H. Emdad, Air Force Flight Dynamics Laboratory (U.S.), Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and United States. Air Force. Systems Command (page images at HathiTrust)
• Vigyan Research Associates: Calculation of high angle of attack aerodynamics of fighter configurations. Vol. III, Unsteady (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1991., 1991), also by C. Edward Lan, Ratikanta Tripathi, S. C. Mehrotra, P. Sundaram, Suei Chin, H. Emdad, Air Force Flight Dynamics Laboratory (U.S.), Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and United States. Air Force. Systems Command (page images at HathiTrust)
• Vigyan Research Associates: Effects of forebody geometry on subsonic boundary-layer stability (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by S. S. Dodbele, Langley Research Center, and Québec) International Conference on Numerical Methods in Laminar and Turbulent Flow (5th : 1987 : Montréal (page images at HathiTrust)
• Vigyan Research Associates: High-speed assembly language (80386/80387) programming for laser spectra scan control and data acquisition providing improved resolution water vapor spectroscopy (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Robert J. Allen, Langley Research Center, and Allen Associates (page images at HathiTrust)
• Vigyan Research Associates: Low-speed investigations of 'Apex Fence' and 'Cavity Flap' concepts on a 60 degree delta configuration (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1987., 1987), also by Dhanvada M. Rao, Charles T. L. Mills, Keith D. Hoffler, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Vigyan Research Associates: Natural laminar flow airfoil design considerations for winglets on low-speed airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by C. P. Van Dam and Langley Research Center (page images at HathiTrust)

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